View source for Messerschmitt Me 163 Komet

{{Short description|German rocket-powered interceptor}}
{{Distinguish|Messerschmitt Bf 163}}
{{Use dmy dates|date=October 2020}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox aircraft
 |name= Me 163 Komet
 |image= File:Messerschmitt Me 163B USAF.jpg
 |image_caption= Me 163B on display at the National Museum of the United States Air Force{{#tag:ref|The small red rectangles on the [[rudder]] and [[elevon]]s are externally fastened [[gust lock]]s to prevent wind damage to the control surfaces while on the ground and are removed before flight.|group=N}}
 |aircraft_type= [[Rocket-powered aircraft|Rocket]] [[Interceptor aircraft|Interceptor]]
 |national_origin= Germany
 |manufacturer= [[Messerschmitt]]
 |designer= [[Alexander Lippisch]]
 |first_flight= 1 September 1941
 |introduction= 1944
 |retired=<!--1944?-->
 |status=
 |primary_user= {{lang|de|[[Luftwaffe]]}}
 |more_users=
 |produced=
 |number_built= ~370<ref>Wilson 1998, p. 121.</ref><ref name = "lepage 249">LePage 2009, p. 249.</ref>
 |unit cost=
 |developed_from=
 |variants=
 |developed_into= [[Messerschmitt Me 263]]
}}

The '''Messerschmitt Me&nbsp;163 Komet''' is a [[Rocket-powered aircraft|rocket-powered]] [[interceptor aircraft]] primarily designed and produced by the German aircraft manufacturer [[Messerschmitt]]. It is the only operational rocket-powered fighter aircraft in history as well as the first piloted aircraft of any type to exceed {{convert|1,000|km/h|mph}} in level flight.

Development of what would become the Me 163 can be traced back to 1937 and the work of the German aeronautical engineer [[Alexander Lippisch]] and the ''[[Deutsche Forschungsanstalt für Segelflug]]'' (DFS). Initially an experimental programme that drew upon traditional [[Glider (aircraft)|glider]] designs while integrating various new innovations such as the rocket engine, the development ran into organisational issues until Lippisch and his team were transferred to Messerschmitt in January 1939. Plans for a propeller-powered intermediary aircraft were quickly dropped in favour of proceeding directly to rocket propulsion. On 1 September 1941, the prototype performed its [[maiden flight]], quickly demonstrating its unprecedented performance and the qualities of its design. Having been suitably impressed, German officials quickly enacted plans that aimed for the widespread introduction of Me 163 [[point-defence]] interceptors across Germany. During December 1941, work began on the upgraded ''Me 163B'', which was optimized for large-scale production.

During early July 1944, German test pilot [[Heini Dittmar]] reached {{convert|1130|km/h|mph|abbr=on}}, an unofficial [[flight airspeed record]] that remained unmatched by [[turbojet]]-powered aircraft until 1953. That same year, the Me 163 began flying operational missions, being typically used to defend against incoming enemy [[Strategic bombing|bombing raids]]. As part of their alliance with the [[Empire of Japan]], Germany provided design schematics and a single Me 163 to the country; this led to the development of the [[Mitsubishi J8M]]. By the end of the conflict, roughly 370 Komets had been completed, most of which were being used operationally. Some of the aircraft's shortcomings were never addressed, and it was less effective in combat than predicted. Capable of a maximum of 7.5 minutes of powered flight, its range fell short of projections and greatly limited its potential. Efforts to improve the aircraft were made (most notably the development of the [[Messerschmitt Me 263]]), but many of these did not see actual combat due to the sustained advance of the [[Allies of World War II|Allied]] powers into Germany in 1945.

After being introduced into service the Me 163 was credited with the destruction of between 9 and 18 Allied aircraft against 10 losses.<ref name="Boyne 1997, p.349">Boyne 1997, p. 349.</ref><ref name="Thompson with Smith p. 233.">Thompson and Smith 2008, p. 233.</ref> Aside from combat losses, numerous Me 163 pilots were killed upon takeoff<ref name=Walker28/> or during testing and training flights.<ref>Ziegler 1976</ref>{{page needed|date=November 2022}} This high loss rate was, at least partially, a result of the later models' use of rocket propellant which was not only highly volatile but also [[corrosive]] and hazardous to humans.<ref name=Walker28>Walker 1983, p. 28.</ref> One noteworthy fatality was that of [[Josef Pöhs]], a German fighter ace and ''[[Oberleutnant]]'' in the ''Luftwaffe'', who was killed in 1943 through exposure to ''[[T-Stoff]]'' in combination with injuries sustained during a failed takeoff that ruptured a fuel line.<ref>Caygill 2006</ref>{{Page needed|date=November 2022}} Besides Nazi Germany, no nation ever made operational use of the Me 163; the only other operational rocket-powered aircraft was the Japanese [[Yokosuka MXY-7 Ohka]] which was a manned flying bomb.

==Development==
===Early work by Alexander Lippisch===
[[File:RRG Raketen-Ente Deutsches Segelflugmuseum 01 2009-05-31.jpg|thumb|Replica of Opel RAK's [[Lippisch Ente]] in ''Deutsches Segelflugmuseum'' as the world's first rocket-powered glider]]
The world's first piloted rocket flights were carried out by the German vehicle manufacturer [[Opel RAK]]. The first flight of such an aircraft, a rocket-modified glider designed by Alexander Lippisch, took place at [[Wasserkuppe]] Mountain on 11 June 1928.<ref>{{cite web |url = https://www.nasa.gov/feature/95-years-ago-first-human-rocket-powered-aircraft-flight |title = 95 years ago: First Human Rocket-Powered Aircraft Flight |publisher = NASA |date = 9 June 2023 }}</ref> Two black powder rockets, designed by [[Friedrich Wilhelm Sander]], were fitted to the aircraft’s rear. Due to the use of a forward canard arrangement, Lippisch named the glider "Ente", German for duck.<ref>{{cite web | url=https://www.airandspaceforces.com/article/0904rocket/ | title=The Rocket Men }}</ref> After a failed first attempt, one rocket finally ignited as intended and the Ente lifted off, test pilot Fritz Stamer flying it for {{Convert | 4900 | ft}} before making a controlled landing. Another flight using both rockets did not go as planned, as one of the two rockets exploded; the damaged aircraft took off due to the active intact rocket, but the control surfaces did not work, and with much of it aflame Stamer barely survived while fire destroyed the Ente.<ref>{{cite web | url=https://www.airandspaceforces.com/article/0904rocket/ | title=The Rocket Men }}</ref>

After the Ente's loss, Fritz von Opel commissioned a dedicated rocket plane, the [[Opel RAK.1]]. It was designed by [[Julius Hatry]], another early Wasserkuppe pioneer, and also equipped with Friedrich Sander's Opel RAK rockets.<ref>{{cite web | url=https://www.airandspaceforces.com/article/0904rocket/ | title=The Rocket Men }}</ref> The first public flight of a rocket plane took place in [[Frankfurt]] on 30 September 1929. Lippisch also continued his independent design work over the following decades, and in particular using rocketry, leading eventually to the Me 163.<ref>{{cite web | url=https://www.airandspaceforces.com/article/0904rocket/ | title=The Rocket Men }}</ref>

===Background===
[[File:Me163Variants.jpg|thumb|Development of the Me 163]]
[[File:HWK 109-509 A.jpg|thumb|A Me 163's [[Walter HWK 109-509|HWK 109-509A]] engine]]
[[File:HWK 109-509.jpg|thumb|Position of the Walter HWK 109-509A-1 rocket motor]]

During 1937, work on what would become the Me 163 commenced,<ref name = "lepage 243">LePage 2009, p. 243.</ref> the initial work was conducted under the aegis of the ''[[Deutsche Forschungsanstalt für Segelflug]]'' (DFS)—the German Institute for the study of [[sailplane]] flight. Their first design was a conversion of the earlier [[Lippisch Delta IV]] known as the '''DFS&nbsp;39''' and used purely as a glider testbed of the [[airframe]]. A larger follow-on version with a small propeller engine started as the [[DFS 194]]. This version used [[wingtip]]-mounted [[rudder]]s that Lippisch felt would cause problems at high speed. Lippisch changed the system of vertical stabilization for the DFS 194's airframe from the earlier DFS 39's wingtip rudders, to a conventional [[vertical stabilizer]] at the rear of the aircraft. The design included a number of features from its origins as a glider, notably a skid used for landings, which could be retracted into the aircraft's keel in flight. For [[takeoff]], a pair of wheels, each mounted onto the ends of a specially designed cross-axle, were needed due to the weight of the fuel, but the wheels, forming a takeoff [[bogie#Bogie (aircraft)|dolly]] under the landing skid, were [[landing gear#Detachable|released shortly after takeoff]].<ref name="wotl 226">Donald 2000, p. 226.</ref><ref name = "lepage 248">LePage 2009, p. 248.</ref>

The designers planned to use the forthcoming Walter R-1-203 ''cold engine'' of {{convert|400|kg|lb|abbr=on}} thrust, which like the self-contained [[Walter HWK 109-500]] ''Starthilfe'' [[RATO]] booster rocket unit, used a [[monopropellant]] consisting of stabilized [[High-test peroxide|HTP]] known by the name [[T-Stoff]]. [[Heinkel]] had also been working with [[Hellmuth Walter]] on his rocket engines, mounting them in the [[Heinkel He 112#Early experiments with rocket propulsion|He 112R]]'s tail for testing – this was done in competition with [[Wernher von Braun]]'s bi-propellant, alcohol/[[LOX]]-fed rocket motors, also with the He 112 as a test airframe – and with the Walter [[Z-Stoff|catalyzed]] HTP propulsion format for the first purpose-designed, liquid-fueled rocket aircraft, the [[Heinkel He 176|He 176]]. Heinkel had also been selected to produce the fuselage for the DFS 194 when it entered production,{{when|date=March 2017}} as it was felt that the monopropellant fuel's high reactivity with organic matter would be too dangerous in a wooden fuselage structure. Work continued under the code name ''Projekt X''.<ref name="ww2-planes">[https://myhobbylife.com/messerschmitt-me-163-komet/ "Messerschmitt Me 163 Komet"]. World War 2 Planes. Retrieved: 22 March 2009.</ref><ref name = "lepage 2478">LePage 2009, pp. 247-248.</ref>

The division of work between DFS and Heinkel led to problems,{{when|date=March 2017}} notably that DFS seemed incapable of building even a [[prototype]] fuselage. Lippisch eventually asked to leave DFS and join [[Messerschmitt]] instead.<ref name = "lepage 247">LePage 2009, p. 247.</ref>{{#tag:ref|In spite of his transference to Messerschmitt, the relationship between Lippisch and [[Willy Messerschmitt]], the company's head, were allegedly strained, nor did the latter have particular enthusiasm for the Me 163 project.<ref name = "dorr 114">Dorr 2013, p. 114.</ref><ref name = "Ziegler 634">Ziegler 1976, pp. 63-64.</ref>|group=N}} On 2 January 1939, Lippisch moved with his team and the partly completed DFS 194 to the Messerschmitt works at [[Augsburg]]. The delays caused by this move allowed the engine development to catch up. Once at Messerschmitt, the team decided to abandon the propeller-powered version and move directly to rocket-power. The airframe was completed in Augsburg and in early 1940 was shipped to receive its engine at [[Peenemünde Airfield|Peenemünde-West]], one of the quartet of ''Erprobungsstelle''-designated military aviation test facilities of the Reich. Although the engine proved to be extremely unreliable, the aircraft had excellent performance, reaching a speed of {{convert|550|km/h|abbr=on}} in one test.<ref name = "Nowarrav 163">Nowarra 1993, p. 163.</ref>

It is important to note that the wing sweep incorporated in the design stemmed from its tailless nature and the need to balance centre of gravity and centre of lift positions for stability purposes. The sweep in both the Me 163 and Me 262 stemmed from these CG and CL issues (heavier than planned engines in the case of the Me 262), not from high speed aerodynamic requirements.<ref>''The Design of the Aeroplane'', Darrol Stinton, 1983, {{ISBN|0 632 01877 1}}, p. 142.</ref>

In the Me&nbsp;163B and -C subtypes, a [[ram-air turbine]] was installed on the extreme nose of the fuselage that, along with a backup [[lead–acid battery]] inside the fuselage that it charged, provided electrical power for various pieces of onboard equipment.<ref name = "heath 220"/> Such apparatus included the [[radio]], [[reflector sight|reflector gunsight]] (either Revi16B, -C, or -D), [[radio direction finder|direction finder]], [[compass]], firing circuits for the twin cannons, as well as some of the lighting for the cockpit instrumentation. Limited battery capacity made the electrical generator necessary.<ref name = "heath 220"/>

The [[airspeed indicator]] averaged readings from two sources: the [[pitot tube]] on the leading edge of the port wing, and a small pitot inlet in the nose, just above the top edge of the underskid channel.{{Citation needed|date=November 2015}} There was a further tapping-off of pressure-ducted air from the pitot tube which also provided the rate of climb indicator with its source.{{Citation needed|date=November 2015}}

The resistance group around the Austrian priest [[Heinrich Maier]] (later executed) had contacts with the Heinkelwerke in [[Jenbach]] in Tyrol, where important components for the Me 163 were also produced. The group supplied location sketches of the production facilities to the Allies, thus greatly aiding Allied bombers in carrying out targeted air strikes against them.<ref>Peter Broucek (2008). ''Die österreichische Identität im Widerstand 1938–1945'', p. 163.</ref><ref>Pirker 2012, p. 252.</ref><ref>Hansjakob Stehle "Die Spione aus dem Pfarrhaus (German: The spy from the rectory)". In: ''Die Zeit'', 5 January 1996.</ref>

===Me 163A===
[[File:Bundesarchiv Bild 146-1972-058-62, Raketenjäger Me 163 A-V4.jpg|thumb|The Me 163A V4 (first prototype) in 1941]]

In early 1941, production of a prototype series, known as the ''Me&nbsp;163'', began. Secrecy was such that [[list of RLM aircraft designations#101-200|the RLM's "GL/C" airframe number]], ''8-163'', was actually that of the earlier [[Messerschmitt Bf 163]]. Three Bf 163-prototypes (V1 to V3) had been built, and it was thought that foreign intelligence services would conclude any reference to the number "163" was for that earlier design. During May 1941, the first prototype '''Me 163A''', V4, was shipped to [[Peenemünde]] to receive the HWK RII-203 engine. By 2 October 1941, Me 163A V4, bearing the radio call sign letters, or ''Stammkennzeichen'', "KE+SW", set a new [[air speed record|world speed record]] of {{convert|1004.5|km/h|mph|abbr=on}}, piloted by [[Heini Dittmar]], with no apparent damage to the aircraft during the attempt.<ref name="Käsemann 1999, pp. 17, 122">Käsemann 1999, pp. 17, 122.</ref><ref>Stüwe 1999, pp. 207, 211, 212, 213.</ref> Some [[postwar aviation]] history publications stated that the Me 163A V3 was thought to have set the record.<ref>Spate and Bateson 1975, p. 55.</ref> The {{convert|1004|km/h|kn mph|abbr=on|lk=on}} record figure would not be officially surpassed until after the war, specifically by the American [[Douglas D-558-1 Skystreak|Douglas D-558-1]] on 20 August 1947. Ten Me&nbsp;163As (V4-V13) were built for pilot training and further tests; these were unarmed.<ref name = "lepage 248"/>

[[File:Me163 Dropping type wheel.jpg|thumb|Me 163B's unsprung [[landing gear#Detachable landing gear|jettisonable main gear]] "dolly" unit]]
[[File:Scheuch-Schlepper.jpg|thumb|Use of the "Scheuch-Schlepper" before an Me 163B's flight (above) and after (below)]]

During testing of the prototype (A-series) aircraft, the [[wikt:jettison|jettisonable]] undercarriage presented a serious problem. The original dollies possessed well-sprung independent suspension for each wheel,<ref>[http://www.nurflugel.com/Nurflugel/Lippisch_Nurflugels/me163a/me163a_r4m.jpg "Lippisch Nürflugels-The Me 163A Komet"]. nurflugel.com. Retrieved: 7 October 2012.</ref> and as the aircraft took off, the large springs rebounded and threw the dolly upward, striking the aircraft. In comparison, the production (B-series) aircraft used much simpler, crossbeam-axled dollies, and relied on the landing skid's [[oleo strut|oleo-pneumatic strut]]<ref name="Hitler's Luftwaffe">{{cite book |title = Hitler's Luftwaffe |last1 = Gunston |first1 = Bill |last2 = Wood |first2 = Tony |year = 1977 |publisher = Salamander Books |pages = 228–229}}</ref> to absorb ground-running impacts during the takeoff run, as well as to absorb the shock of landing. If the hydraulic cylinder was malfunctioning, or the skid mistakenly left during a landing procedure in the "locked and lowered" position (as it had to be for takeoff), the impact of a hard touchdown on the skid could cause back injuries to the pilot.<ref>{{cite web |url = https://airandspace.si.edu/collection-objects/messerschmitt-me-163b-1a-komet/nasm_A19530072000 |title = Smithsonian National Air and Space Museum - Collections - Messerschmitt Me 163B-1a Komet - Long Description |author = <!--Staff writer(s); no by-line.--> |website = airandspace.si.edu |publisher = Smithsonian National & Space Museum |access-date = 2 January 2016 |quote = The Komet's landing gear also proved troublesome, with numerous pilots suffering back injuries as a result of the skid failing to extend properly or failing upon touchdown. Even when the skid operated properly, landings were always without power and at high speed, requiring the utmost care on the part of the pilot to prevent the aircraft from overturning on soft ground.}}</ref><ref name = "lepage 456">LePage 2009, pp. 45-46.</ref>

Once on the ground, the aircraft had to be retrieved by a ''Scheuch-Schlepper'', a converted small agricultural vehicle,<ref>{{cite web |url = https://robdebie.home.xs4all.nl/me163/equipment09.htm |title = Me 163 ground equipment: Scheuch-Schlepper |website = robdebie.home.xs4all.nl}}</ref> originally based on the concept of the [[two-wheel tractor]], carrying a detachable third swiveling wheel at the extreme rear of its design for stability in normal use—this swiveling third wheel was replaced with a pivoting, special retrieval trailer that rolled on a pair of short, triple-wheeled [[continuous track]] setups (one per side) for military service wherever the ''Komet'' was based. This retrieval trailer usually possessed twin trailing lifting arms, that lifted the stationary aircraft off the ground from under each wing whenever it was not already on its twin-wheel dolly main gear, as when the aircraft had landed on its ventral skid and tailwheel after a mission.<ref>de Bie, Rob.[https://robdebie.home.xs4all.nl/me163/equipment08.htm "Me 163 ground equipment: Scheuch-Schlepper"]. Me 163 Komet Website. Retrieved: 7 October 2012.</ref> Another form of trailer, known also to have been trialled with the later B-series examples, was tried during the ''Komet''{{'}}s test phase, which used a pair of sausage-shaped [[air bag]]s in place of the lifting arms and could also be towed by the ''Scheuch-Schlepper'' tractor, inflating the air bags to lift the aircraft.<ref>{{cite AV media |people = United States Army Air Forces, Wright Field Air Materiel Command, Film WF 69-28 |year = 1944 |title = WW2: Flight test of German Aeronautical equipment -- Me 163 (1944) |url = https://www.youtube.com/watch?v=tBbMaxsTh8c |archive-url=https://web.archive.org/web/20140517032700/http://www.youtube.com/watch?v=tBbMaxsTh8c&NR=1 |archive-date = 17 May 2014 |time = 0:33 seconds in |publisher = USAAF |url-status = dead}}</ref><ref>de Bie, Rob.[https://robdebie.home.xs4all.nl/me163/wh05-07.htm "Me 163B "White 05" of Erprobungskommando 16"]. Me 163 Komet Website. Retrieved: 7 October 2012.</ref> The three-wheeled ''Scheuch-Schlepper'' tractor used for the task was originally meant for farm use, but such a vehicle with a specialized trailer—which could also lift the Me 163's airframe completely clear of the ground to effect the recovery as a normal part of the Me 163's intended use—was required as the ''Komet'' was unpowered after exhausting its rocket propellants, and lacked main wheels after landing, from the jettisoning of its "dolly" main gear at takeoff.<ref>de Bie, Rob.[https://robdebie.home.xs4all.nl/me163/equipment08.htm "Me 163 ground equipment: Scheuch-Schlepper"]. Me 163 Komet Website. Retrieved: 5 December 2012.</ref>

During flight testing, the superior gliding capability of the ''Komet'' proved detrimental to safe landing. As the now un-powered aircraft completed its final descent, it could rise back into the air with the slightest updraft. Since the approach was unpowered, there was no opportunity to make another landing pass. For production models, a set of landing [[flap (aircraft)|flaps]] allowed somewhat more controlled landings. This issue remained a problem throughout the program. Nevertheless, the overall performance was tremendous, and plans were made to put Me 163 squadrons all over Germany in {{convert|40|km|mi|adj=mid|rings}} around any potential target.{{#tag:ref|According to the historian Robert F. Dorr, while [[Hermann Göring]], the head of the Luftwaffe, was a keen proponent of the Me 163, [[Adolf Hitler]] was unimpressed by the aircraft, instead favouring the jet-powered [[Messerschmitt Me 262]] amongst other projects.<ref name = "dorr 14">Dorr 2013, p. 14.</ref>|group=N}} However, while the development of an operational version was encouraged, the Me 163 programme was not assigned the highest priority due to competition from other projects; this lack of focus protracted its development.<ref name = "Ziegler 567">Ziegler 1976, pp. 56-57.</ref>

===Me 163B===
[[File:Me163efJM.jpg|thumb|Me&nbsp;163&nbsp;B-1a at the [[National Museum of Flight]] in [[East Fortune]], Scotland]]

In December 1941, work on an upgraded design began. A simplified construction format for the airframe was deemed necessary, as the Me 163A version was not truly optimized for large-scale production. The result was the '''Me 163B''' subtype that had the desired, more mass-producible fuselage, wing panel, retractable landing skid and [[tailwheel]] designs with the previously mentioned unsprung dolly takeoff gear, and a generally one-piece conical nose for the forward fuselage which could incorporate a [[ram air turbine|turbine]] for supplementary electrical power while in flight, as well as a one-piece, perimeter frame-only hinged canopy for ease of production.<ref>de Bie, Rob. [https://robdebie.home.xs4all.nl/me163/production.htm "Me 163B Komet - Me 163 Production"]. xs4all.nl. Retrieved: 5 December 2012.</ref>{{Failed verification|date=January 2014}}<ref name = "heath 220">Heath 2022, p. 220.</ref>
[[File:ME 163 landing skid extended.jpg|thumb|Landing skid of a Messerschmitt Me 163B shown extended for takeoff, with the take-off dolly attached.]]

Meanwhile, Walter had started work on the newer [[HWK 109-509]] bipropellant ''hot engine'', which added a fuel of [[hydrazine|hydrazine hydrate]] and [[methanol]], designated ''{{Nowrap|[[C-Stoff]]}}'', that burned with the oxygen-rich exhaust from the {{Nowrap|[[T-Stoff]]}}, used as the oxidizer, for added thrust. The new powerplant and numerous detail design changes meant to simplify production over the general A-series airframe design resulted in the significantly modified '''Me 163B''' of late 1941. Due to the ''[[Reich Air Ministry|Reichsluftfahrtministerium]]'' requirement that it should be possible to [[throttle]] the engine, the original power plant grew complicated and lost reliability.{{citation needed|date=March 2017}} The ''Komet'' carried no more than {{Convert|437|gal|L}} of fuel, which was exhausted in 4 to 7 minutes, limiting its flight radius to {{Convert|25|mi}}.<ref name="Walker28" />

The fuel system was particularly troublesome, as leaks incurred during hard landings easily caused fires and explosions. Metal fuel lines and fittings, which failed in unpredictable ways, were used as this was the best technology available. Both fuel and oxidizer were toxic and required extreme care when loading in the aircraft, yet there were occasions when ''Komets'' exploded on the tarmac from the propellants' [[hypergolic]] nature. Both propellants were clear fluids, and different tanker trucks were used for delivering each propellant to a particular ''Komet'' aircraft, usually the ''C-Stoff'' hydrazine/methanol-base fuel first. For safety purposes, the truck left the immediate area of the aircraft following its delivery and capping off of the ''Komet''{{-'}}s fuel tanks from a rear located dorsal fuselage filling point just ahead of the ''Komet''{{-'}}s vertical stabilizer. Then, the other tanker truck carrying the very reactive T-Stoff hydrogen peroxide oxidizer would deliver its load through a different filling point on the ''Komet''{{-'}}s dorsal fuselage surface, located not far behind the rear edge of the canopy.<ref>{{cite web |url = https://robdebie.home.xs4all.nl/me163/equipment38.htm |title = Me 163 ground equipment: Opel Blitz T-Stoff tanker |last = de Bie |first = Rob |website = robdebie.home.xs4all.nl/me163.htm |access-date = 4 October 2013}}</ref>

The corrosive nature of the liquids, especially for the T-Stoff oxidizer, required special protective gear for the pilots. To help prevent explosions, the engine and the propellant storage and delivery systems were frequently and thoroughly hosed down and flushed with water run through the propellant tanks and the rocket engine's propellant systems before and after flights, to clean out any remnants.<ref>{{cite episode |title = Messerschmitt Me 163 Komet |series = Wings of the Luftwaffe |network = Discovery Military Channel |time = 44:09 (30:25 minutes) |language = en}}</ref> The relative "closeness" to the pilot of some 120 litres (31.7 US gal) of the chemically active T-Stoff oxidizer, split between two auxiliary oxidizer tanks of equal volume to either side within the lower flanks of the cockpit area—besides the main oxidizer tank of some 1,040-litre (275 US gal) volume just behind the cockpit's rear wall, could present a serious or even fatal hazard to a pilot in a fuel-caused mishap.<ref name="Gunston and Wood 1977, p. 228">Gunston and Wood 1977, p. 228.</ref>

Two prototypes were followed by 30 '''Me&nbsp;163&nbsp;B-0''' pre-production aircraft armed with two 20&nbsp;mm [[MG 151 cannon|MG 151/20 cannon]] and some 400 '''Me&nbsp;163&nbsp;B-1''' production aircraft armed with two 30&nbsp;mm (1.18-inch) [[MK 108 cannon]]s, but which were otherwise similar to the B-0. Early in the war, when German aircraft firms created versions of their aircraft for export purposes, the '''a''' was added to export (''ausland'') variants (B-1a) or to foreign-built variants (Ba-1) but for the Me 163, there were neither export nor a foreign-built version. Later in the war, the "a" and successive letters were used for aircraft using different engine types: as Me&nbsp;262&nbsp;A-1a with Jumo engines, Me&nbsp;262&nbsp;A-1b with BMW engines. As the Me 163 was planned with<ref>{{cite web |url = https://robdebie.home.xs4all.nl/me163/bmw03.htm |title = Me 163B powered by BMW P 3330A |website = robdebie.home.xs4all.nl}}</ref> an alternative BMW P3330A rocket engine, it is likely the "a" was used for this purpose on early examples. Only one Me 163, the V10, was tested with the BMW engine, so this designation suffix was soon dropped. The Me&nbsp;163&nbsp;B-1a did not have any wingtip "washout" built into it, and as a result, it had a much higher [[critical Mach number]] than the Me&nbsp;163&nbsp;B-1.<ref>Stüwe 1999, p. 254.</ref>

The Me&nbsp;163B had very docile landing characteristics, mostly due to its integrated [[leading edge slot]]s, located directly forward of the [[elevon]] control surfaces, and just behind and at the same angle as the wing's [[leading edge]]. It would neither stall nor spin. One could fly the ''Komet'' with the stick full back, and have it in a turn and then use the rudder to take it out of the turn, and not fear it snapping into a spin. It would also slip well. Because the Me 163B's airframe design was derived from glider design concepts, it had excellent gliding qualities, and the tendency to continue flying above the ground due to [[ground effect in aircraft|ground effect]]. On the other hand, making a too close turn from base onto final, the sink rate would increase, and one could quickly lose altitude and come in short. Another main difference from a propeller-driven aircraft is that there was no slipstream over the rudder. On takeoff, one had to attain the speed at which the aerodynamic controls become effective—about {{convert|129|km/h|mph|abbr=on}}—and that was always a critical factor. Pilots accustomed to flying propeller-driven aircraft had to be careful that the control stick was not somewhere in the corner when the control surfaces began working. These, like many other specific Me 163 problems, would be resolved by specific training.<ref>{{cite web |url=http://homepage.ntlworld.com/andrew.walker6/komet/flight/flight2.htm|archive-url=https://web.archive.org/web/20111221090428/http://homepage.ntlworld.com/andrew.walker6/komet/flight/flight2.htm |archive-date=21 December 2011 |title = Komet 163 - Chief test pilot Rudy Opitz tells it like it was |last = Atwood |first = Tom |date = 21 July 2001 }}</ref>

The performance of the Me 163 far exceeded that of contemporary piston engine fighters. At a speed of over {{convert|320|km/h|mph|abbr=on}} the aircraft would take off, in a so-called {{-"}}''scharfer Start''{{-"}} ("hot start") from the ground, from its two-wheeled dolly. The aircraft would be kept at level flight at low altitude until the best climbing speed of around {{convert|676|km/h|mph|abbr=on}} was reached, at which point it would jettison the dolly, retract its extendable skid using a knob-topped release lever just forward of the throttle<ref>{{cite web |url = http://homepage.ntlworld.com/andrew.walker6/komet/flight/flight2.htm |title = Komet 163 - Chief test pilot Rudy Opitz tells it like it was |last = Atwood |first = Tom |date = 21 July 2001 |page = 2 |publisher = Flight Journal |access-date = 15 February 2017 |quote = From caption of photo on page 2 of article: "...(4) Five-position throttle: off, ground idle, flight idle, cruise, max power. (5) Undercarriage extension/retraction [lever]. |url-status = dead |archive-url = https://web.archive.org/web/20111221090428/http://homepage.ntlworld.com/andrew.walker6/komet/flight/flight2.htm |archive-date = 21 December 2011}}</ref> (as both levers were located atop the cockpit's portside 120-litre T-Stoff oxidizer tank) that engaged the aforementioned pneumatic cylinder,<ref name="Hitler's Luftwaffe"/> and then pull up into a 70° angle of climb, to a bomber's altitude. It could go higher if required, reaching {{convert|12000|m|ft|abbr=on}} in an unheard-of three minutes. Once there, it would level off and quickly accelerate to around {{convert|880|km/h|mph|abbr=on}} or faster, which no [[Allies of World War II|Allied]] fighter could match. The usable Mach number was similar to that of the Me 262, but because of the high thrust-to-drag ratio, it was much easier for the pilot to lose track of the onset of severe compressibility and risk loss of control. A Mach warning system was installed as a result. The aircraft was remarkably agile and docile to fly at high speed. According to Rudolf Opitz, chief test pilot of the Me 163, it could "fly circles around any other fighter of its time".{{citation needed|date=March 2017}}

By this point, Messerschmitt was completely overloaded with production of the [[Messerschmitt Bf 109]] and attempts to bring the [[Messerschmitt Me 210|Me 210]] into service. Production in a dispersed network was handed over to Klemm, but quality control problems were such that the work was later given to Junkers, who were, at that time, underworked. As with many German designs of World War II's later years, parts of the airframe (especially the wings) were made of wood by furniture manufacturers. The older Me 163A and first Me 163B prototypes were used for training. It was planned to introduce the '''Me 163S''', which removed the rocket engine and tank capacity and placed a second seat for the instructor above and behind the pilot, with his own canopy. The Me 163S would be used for glider landing training, which as explained above, was essential to operate the Me 163. It appears that the Me 163S was produced via the conversion of the earlier Me 163B series prototypes.{{citation needed|date=March 2017}}

In service, the Me 163 turned out to be difficult to use against enemy aircraft. Its tremendous speed and climb rate meant a target was reached and passed in a matter of seconds. Although the Me 163 was a stable gun platform, it required excellent marksmanship to bring down an enemy bomber. The ''Komet'' was equipped with two 30&nbsp;mm (1.18&nbsp;inch) [[MK 108 cannon]]s that had a relatively low muzzle velocity of 540 meters per second (1,772&nbsp;feet/sec), and were accurate only at short range, making it almost impossible to hit a slow moving bomber. Four or five hits were typically needed to take down a [[Boeing B-17 Flying Fortress|B-17]].<ref>{{cite web |url = https://sofrep.com/news/weapons-from-the-second-world-war-that-failed-miserably/ |title = Weapons From The Second World War That Failed Miserably |publisher = sofrep.com |date = 21 March 2022}}</ref>

Innovative methods were employed to help pilots achieve kills. The most promising was a weapon called the [[Jagdfaust|''Sondergerät 500 Jägerfaust'']]. This included 10 single-shot, short-barreled 50&nbsp;mm (2-inch) guns pointing upwards, similar to ''[[Schräge Musik]]''. Five were mounted in the wing roots on each side of the aircraft. A [[photocell]] in the upper surface of the ''Komet'' triggered the weapons by detecting the change in brightness when the aircraft flew under a bomber. As each shell shot upwards, the disposable gun barrel that fired it was ejected downwards, thus making the weapon [[recoilless rifle|recoilless]]. It appears that this weapon was used in combat only once, resulting in the destruction of a Lancaster bomber on 10 April 1945.<ref>{{cite web |url = https://robdebie.home.xs4all.nl/me163/weapons01.htm |title = Komet weapons: SG500 Jägerfaust |website = robdebie.home.xs4all.nl}}</ref><ref>Ethell and Price 1979, pp. 133–135.</ref><ref>Ethell 1978, p. 140.</ref><ref>Spick 2006, p. 191.</ref>

===Later versions===
[[File:Walter HWK 509B-1 USAF.jpg|thumb|A preserved HWK 109-509B "cruiser" twin-chamber rocket motor ([[National Museum of the United States Air Force]])]]
[[File:Me163C 2.JPG|thumb|Model of the Me 163C]]
[[File:Me163D 1.JPG|thumb|Model of the unbuilt Me 163D, erroneously marked with the Me 163B V18's markings for this airframe design]]

The biggest concern about the design was the short flight time, which never met the projections made by Walter. Being capable of a maximum of 7.5 minutes of powered flight (which was only roughly 25% of the 30-minute combat time that the "light-class" [[Heinkel He 162]]A ''Spatz'' single-BMW 003 jet fighter possessed),<ref>Gunston and Wood 1977, pp. 194–195.</ref> when the Komet entered combat in April 1945; the solely rocket-powered Me 163B fighter truly was a dedicated [[point defense]] [[interceptor aircraft|interceptor]]. To improve this, the Walter firm began developing two more advanced versions of the 509A rocket engine, the 509B and C, each with two separate combustion chambers of differing sizes, one above the other, for greater efficiency.<ref name="control panel">Wiedmer, Erwin. [https://www.deutscheluftwaffe.de/Panelnachbau/Erwin/Me163V18Nachbau.htm "Me 163 B V18 control panel"] {{webarchive|url=https://web.archive.org/web/20160410051913/http://www.deutscheluftwaffe.de/Panelnachbau/Erwin/Me163V18Nachbau.htm |date=10 April 2016}}. deutscheluftwaffe.de. Retrieved: 31 August 2011.</ref> The B-version possessed a main combustion chamber—usually termed in German as a ''Hauptofen'' on these dual-chamber subtypes—with an exterior shape much like that on the single chamber 509A version, with the C-version having a forward chamber shape of a more cylindrical nature, designed for a higher top thrust level of some 2,000&nbsp;kg (4,410&nbsp;lb) of thrust, while simultaneously dropping the use of the cubic-shape frame for the forward engine propellant flow/turbopump mechanisms as used by the earlier -A and -B versions.<ref>[http://www.walterwerke.co.uk/walter/me163c1.htm "Me.163B - The Walter RII-211, HWK 109-509.B"]. The Hellmuth Walter Website. Retrieved: 28 July 2013.</ref><ref>[http://www.walterwerke.co.uk/walter/me163c2.htm "Junkers Ju.248 (aka Me.263) The Walter RII-211, HWK 109-509.C"]. The Hellmuth Walter Website. Retrieved: 28 July 2013.</ref> The 509B and 509C rocket motors' main combustion chambers were supported by the thrust tube exactly as the 509A motor's single chamber had been. They were tuned for high power for takeoff and climb. The added, smaller volume lower chamber on the two later models, nicknamed the ''Marschofen'' with approximately {{convert|400|kg|lb|abbr=on}} of thrust at its top performance level, was intended for more efficient, lower power cruise flight. These HWK 109–509B and C motors would improve endurance by as much as 50%. Two 163 Bs, models V6 and V18, were experimentally fitted with the lower-thrust B-version of the new twin-chamber engine (mandating twin combustion chamber pressure gauges on the instrument panel<ref>{{cite web |url = https://www.deutscheluftwaffe.de/Flugzeuge/Projekte/Me163-C/Me%20163C.htm#Risszeichnung |title = Projekt Me 163 "C" - Instrumentbrett der Me 163C mit Marschofen (in German) |first = Erwin |last = Wiedmer |website = deutscheluftwaffe.de |access-date = 3 January 2016 |url-status=dead |archive-url=https://web.archive.org/web/20160125154712/http://www.deutscheluftwaffe.de/Flugzeuge/Projekte/Me163-C/Me%20163C.htm#Risszeichnung |archive-date=25 January 2016}}</ref> of any ''Komet'' equipped with them), a retractable tailwheel, and tested in spring 1944.<ref name="control panel"/><ref>[http://www.walterwerke.co.uk/walter/me163c1a.htm "Me.163B V6 and V18 - The Walter RII-211, HWK 109-509.B"]. The Hellmuth Walter Website. Retrieved: 28 July 2013.</ref>

The main ''Hauptofen'' combustion chamber of the 509B engine used for the B V6 and V18 occupied the same location as the A-series' engine did, with the lower ''Marschofen'' cruise chamber housed within the retractable tailwheel's appropriately widened ventral tail fairing. On 6 July 1944, the Me 163B V18 (VA+SP), like the B V6 basically a standard production Me 163B airframe outfitted with the new, twin-chamber "cruiser" rocket motor with the aforementioned airframe modifications beneath the original rocket motor orifice to accept the extra combustion chamber, set a new unofficial world speed record of {{convert|1130|km/h|mph|0|abbr=on}}, piloted by Heini Dittmar, and landed with almost all of the vertical rudder surface broken away from flutter.<ref name="Käsemann 1999, pp. 17, 122"/><ref>de Bie, Rob. [https://robdebie.home.xs4all.nl/me163/production.htm "Me 163B Komet - Me 163 Production - Me 163B: Werknummern list"]. robdebie.home. Retrieved: 28 July 2013.</ref><ref>[http://www.walterwerke.co.uk/walter/me163c1a.htm "Me 163"]. walterwerke.co.uk. Retrieved: 28 August 2010.</ref> This record was not broken in terms of absolute speed until 6 November 1947 by [[Chuck Yeager]] in [[list of X-1 flights|flight number 58]] that was part of the [[Bell X-1]] test program, with a {{convert|1434|km/h|mph|abbr=on}}, or Mach 1.35 supersonic speed, recorded at an altitude of nearly {{convert|14820|m|ft|abbr=on}}.{{#tag:ref|[[List of X-1 flights]]|group=N}} However, it is unclear if Dittmar's flight achieved sufficient altitude for its speed to be considered supersonic, as the X-1 did.

The X-1 never exceeded Dittmar's speed from a normal runway {{-"}}''scharfer Start''{{-"}} liftoff. Heini Dittmar had reached the {{convert|1130|km/h|mph|0|abbr=on}} performance, after a normal "hot start" ground takeoff, without an air drop from a mother ship. [[Neville Duke]] exceeded Heini Dittmar's record mark roughly {{frac|5|1|2}} years after Yeager's achievement (and some 263&nbsp;km/h short of it) on 31 August 1953 with the [[Hawker Hunter|Hawker Hunter F Mk3]] at a speed of {{convert|1171|km/h|mph|abbr=on}}, after a normal ground start.<ref>Käsemann 1999, pp. 47, 128.</ref>{{#tag:ref|Test Pilot [[Neville Duke]] set a world record on 7 September 1953.|group=N}} Postwar experimental aircraft of the aerodynamic configuration that the Me 163 used, were found to have serious stability problems when entering transonic flight, like the similarly configured, and [[turbojet]] powered, Northrop [[X-4 Bantam]] and [[de Havilland DH 108]],<ref>{{cite book |title = Wings on my Sleeve |last = Brown |first = Eric |author-link = Eric Brown (pilot) |publisher = Weidenfeld & Nicolson |year = 2006 |isbn = 978-0-297-84565-2 |pages = 147 & 184}}</ref> which made the V18's record with the Walter 509B "cruiser" rocket motor more remarkable.

Waldemar Voigt of Messerschmitt's ''Oberammergau'' project and development offices started a redesign of the 163 to incorporate the new twin-chamber Walter rocket engine, as well as fix other problems. The resulting '''Me 163C''' design featured a larger wing through the addition of an insert at the wing root, an extended fuselage with extra tank capacity through the addition of a plug insert behind the wing, a ventral fairing whose aft section possessed a retractable tailwheel design closely resembling that pioneered on the Me 163B V6, and a new pressurized cockpit topped with a bubble canopy for improved visibility, on a fuselage that had dispensed with the earlier B-version's dorsal fairing. The additional tank capacity and cockpit pressurization allowed the maximum altitude to increase to {{convert|15850|m|ft|abbr=on}}, as well as improving powered time to about 12 minutes, almost doubling combat time (from about five minutes to nine). Three '''Me&nbsp;163&nbsp;C-1a''' prototypes were planned, but it appears only one was flown, but without its intended engine.<ref>Green 1970, p. 604.</ref>

By this time the project was moved to Junkers. There, a new design effort under the direction of [[Heinrich Hertel]] at Dessau attempted to improve the ''Komet''. The Hertel team had to compete with the Lippisch team and their Me 163C. Hertel investigated the Me 163 and found it was not well suited for mass production and not optimized as a fighter aircraft, with the most glaring deficiency being the lack of retractable landing gear. To accommodate this, what would eventually become the Me 263 V1 prototype would be fitted with the desired tricycle gear, also accommodating the twin-chamber Walter rocket from the start—later it was assigned to the Ju 248 program.<ref>[http://www.klueser.eu/Me163.php German site about the Me 163]. Retrieved: 5 August 2011</ref><ref>Dressel, Griehl. ''Die deutschen Raketenflugzeuge 1935–1945'' (in German). Augsburg, Germany: Weltbild Verlag, 1995.</ref><ref name = "lepage 249"/>

The resulting ''Junkers Ju 248'' used a three-section fuselage to ease construction. The V1 prototype was completed for testing in August 1944, and was glider-tested behind a [[Junkers Ju 188]]. Some sources state that the Walter 109–509C engine was fitted in September, but it was probably never tested under power. At this point the RLM reassigned the project to Messerschmitt, where it became the [[Messerschmitt Me 263]]. This appears to have been a formality only, with Junkers continuing the work and planning production.<ref>Green 1971, pp. 112–114.</ref> By the time the design was ready to go into production, the plant where it was to be built was overrun by [[Soviet Union|Soviet]] forces. While it did not reach operational status, the work was briefly continued by the [[Soviet Union|Soviet]] [[Mikoyan-Gurevich]] (MiG) design bureau as the [[Mikoyan-Gurevich I-270]].<ref>Green 1971, pp. 150–151.</ref>

==Operational history==
[[File:Me-163Shootdown.JPG|thumb|A Me 163 being shot down, as seen from [[USAAF]] [[Republic P-47 Thunderbolt|P-47]] gun camera]]

The initial test deployment of the Me 163A, to acquaint prospective pilots with the world's first rocket-powered fighter, occurred with ''Erprobungskommando 16'' (Service Test Unit 16, EK 16), led by ''Major'' [[Wolfgang Späte]] and first established in late 1942, receiving their eight A-model service test aircraft by July 1943. Their initial base was as the ''Erprobungsstelle'' (test facility) at the [[Peenemünde-West]] field. They departed permanently the day after an RAF bombing raid on the area on 17 August 1943, moving southwards, to the base at [[Anklam]], near the Baltic coast. Their stay was brief, as a few weeks later they were placed in northwest Germany, based at the military airfield at [[Bad Zwischenahn]]<!-- (at {{Coord|53|12|16.48|N|7|59|37.20|E}}) This seems better to have at the airbase page than here--> from August 1943 to August 1944.<ref name = "Ziegler 68">Ziegler 1976, p. 68.</ref> EK 16 received their first B-series armed Komets in January 1944, and was ready for action by May while at Bad Zwischenahn. ''Major'' Späte flew the first-ever Me 163B combat sortie on 13 May 1944 from the Bad Zwischenahn base, with the Me 163B armed prototype (V41), bearing the ''Stammkennzeichen'' PK+QL.<ref>{{cite web |url = https://robdebie.home.xs4all.nl/me163/units.htm |title = Me 163B Komet - Me 163 units - Erprobungskommando 16 (EK 16) |last1 = de Bie |first1 = Rob |website = robdebie.home.xs4all.nl/me163.htm |publisher = Rob de Bie |access-date = 28 September 2013}}</ref><ref name = "lepage 249"/>

During early 1944, routine [[aerial reconnaissance]] flights over German aerodromes had made the Allies aware of the existence of the Me 163,<ref name="Ziegler 1134">Ziegler 1976, pp. 113-114.</ref> but as EK 16 commenced small-scale combat operations in May 1944, the Me 163B's unsurpassed velocity was something Allied fighter pilots were at a loss to counter. The ''Komets'' attacked singly or in pairs, often even faster than the intercepting fighters could dive. A typical Me 163 tactic was to fly vertically upward through the bombers at {{convert|9000|m|ft|abbr=on}}, climb to {{convert|10700|-|12000|m|ft|abbr=on}}, then dive through the formation again, firing as they went. This approach afforded the pilot two brief chances to fire a few rounds from his cannons before gliding back to his airfield. The pilots reported it was possible to make four passes on a bomber, but only if it was flying alone.<ref name="Späte p252">Späte 1989, p. 252.</ref> According to the historian Mano Ziegler, German officials were allegedly considering using the Me 163 to directly ram into enemy aircraft in suicide attacks; this desperate tactic was never actually used.<ref name = "Ziegler 57">Ziegler 1976, p. 57.</ref> 

Prospective Me163 pilots received training in ''[[DFS Habicht|Stummelhabicht]]'' gliders which, like the Komet, had a short wingspan and high landing speed.<ref name="ZieglerM2">Ziegler 1976, p. 11, 154.</ref> Training included gunnery practice with a machine pistol mounted in the glider nose.<ref>{{cite book |last1 = Volmar |first1 = Joe |title = I Learned to Fly for Hitler |date = 1999 |publisher = Kron Publications |location = Dundee |isbn = 9780967138909 |pages = 145, 167–173}}</ref> As the cockpit was unpressurized, the operational ceiling was limited by what the pilot could endure for several minutes while breathing oxygen from a mask, without losing consciousness. Pilots underwent [[altitude chamber]] training to harden them against the rigors of operating in the thin air of the [[stratosphere]] without a [[pressure suit]]. Special low fiber diets were prepared for pilots, as gas in the [[Human gastrointestinal tract|gastrointestinal tract]] would expand rapidly during ascent.<ref name="ZieglerM">Ziegler 1976, p. 3-4.</ref>

Following the initial combat trial missions of the Me 163B with EK 16, during the winter and spring of 1944 ''Major'' Späte formed the Luftwaffe's first dedicated Me 163 fighter wing, [[Jagdgeschwader 400|''Jagdgeschwader'' 400]] (JG 400), in [[Brandis]], near [[Leipzig]].<ref name = "dorr 10910">Dorr 2013, pp. 109-110.</ref> JG 400's purpose was to provide additional protection for the [[Leuna]] [[synthetic fuel|synthetic gasoline]] works which [[Oil Campaign chronology of World War II|were raided frequently]] during almost all of 1944. A further group was stationed at [[Stargard Szczeciński|Stargard]] near [[Stettin]] to protect the large synthetic fuel plant at Pölitz (today [[Police, West Pomeranian Voivodeship|Police, Poland]]). Further defensive units of rocket fighters were planned for [[Berlin]], the [[Ruhr]], and the [[German Bight]].<ref name="Galland 1957, p.251">Galland 1957, p. 251.</ref>

[[File:Me 163 at Melbourne c1950.jpg|thumb|Typical appearance of a ''Komet'' after landing, waiting for the airfield's ''Scheuch-Schlepper'' tractor and lifting trailer to tow it back for reattachment of its "dolly" maingear]]

The first actions involving the Me 163B in regular Luftwaffe active service occurred on 28 July 1944, from I./JG 400's base at [[Brandis]], when two USAAF B-17 Flying Fortress were attacked without confirmed kills. Combat operations continued from May 1944 to spring 1945. During this time, there were nine confirmed kills with ten Me 163s lost. ''[[Feldwebel]]'' Siegfried Schubert was the most successful pilot, with three bombers to his credit.<ref>Späte 1989, p. XII.</ref> Each engagement would see as many as a dozen Me 163s at a time launched to challenge the B-17s.<ref name = "dorr 136">Dorr 2013, p. 136.</ref>

Allied fighter pilots quickly observed the short duration of the Me 163's powered flight, and adapted their tactics to take advantage of this. The fighters would delay engaging until after the engine had exhausted its propellant before pouncing on the unpowered ''Komet''. Even with this handicap, the aircraft was extremely manoeuvrable in gliding flight and thus was not a straightforward target to down. Another Allied method of engagement was to attack the airfields from which the Komets operated, performing strafing runs upon them after the Me 163s had landed. Due to the skid-based landing gear system, the Komet was immobile until the ''Scheuch-Schlepper'' tractor could back the trailer up to the nose of the aircraft, place its two rear arms under the wing panels, and jack up the trailer's arms to hoist the aircraft off the ground or place it back on its take-off dolly to tow it back to its maintenance area.<ref>Ethell 1978, pp. 94–144.</ref>

At the end of 1944, 91 aircraft had been delivered to JG 400, but a persistent lack of fuel had kept most of them grounded. It was clear that the original plan for a huge network of Me 163 bases would never be realized. Up to that point, JG 400 had lost only six aircraft due to enemy action. Nine Me 163s had been lost to other causes, remarkably few for such a revolutionary and technologically advanced aircraft. Into early 1945, the type continued to be flown to defend high priority targets, such as the [[Mercedes-Benz Group|Daimler Benz]] tank factory in Berlin.<ref name = "dorr 213">Dorr 2013, p. 213.</ref> In the final days of [[Nazi Germany]], the Me 163 was given up in favor of the more successful [[Messerschmitt Me 262|Me&nbsp;262]]. At the beginning of May 1945, Me 163 operations were stopped, the JG 400 disbanded, and many of its pilots sent to fly Me 262s.<ref name="Späte p252"/>

In any operational sense, the ''Komet'' was a failure. Although it shot down sixteen aircraft, mainly four-engined bombers, it did not warrant the effort put into the project. Due to fuel shortages late in the war, few went into combat, and it took an experienced pilot with excellent shooting skills to achieve kills. The ''Komet'' also inspired later rocket planes such as the vertical-launch [[Bachem Ba 349 Natter]]. Ultimately, the point defense role that the Me 163 played would be taken over by the [[surface-to-air missile]], Messerschmitt's own example being the [[Enzian]].<ref name = "lepage 249"/>

===Postwar flight===

Captain [[Eric Brown (pilot)|Eric Brown]] RN, Chief Naval [[test pilot|Test Pilot]] and commanding officer of the [[No. 1426 Flight RAF|Captured Enemy Aircraft Flight]], who tested the Me 163 at the [[Royal Aircraft Establishment]] at [[Farnborough Airfield|Farnborough]], said, "The Me 163 was an aeroplane that you could not afford to just step into the aircraft and say 'You know, I'm going to fly it to the limit.' You had very much to familiarise yourself with it because it was state-of-the-art and the technology used."<ref name="Thompson with Smith pp. 231-232.">Thompson with Smith 2008, pp. 231–232.</ref> Acting unofficially, after a spate of accidents involving Allied personnel flying captured German aircraft resulted in official disapproval of such flights, Brown was determined to fly a powered Komet. On around 17 May 1945, he flew an Me 163B at Husum with the help of a cooperative German ground crew, after initial towed flights in an Me 163A to familiarise himself with the handling.<ref name="Brown">Brown 2006, p. 110-111.</ref>

The day before the flight, Brown and his ground crew had performed an engine run on the chosen Me 163B to ensure that everything was running correctly, the German crew being apprehensive should an accident befall Brown, until being given a disclaimer signed by him to the effect that they were acting under his orders. On the rocket-powered {{-"}}''scharfer-start''{{-"}} takeoff the next day, after dropping the takeoff dolly and retracting the skid, Brown later described the resultant climb as "like being in charge of a runaway train", the aircraft reaching {{Convert | 32000 | ft}} altitude in 2 minutes, 45 seconds. During the flight, while practicing attacking passes at an American B-17 bomber, he was surprised at how well the Komet accelerated in the dive with the engine shut down. When the flight was over Brown had no problems on the approach to the airfield; apart from the rather restricted view from the cockpit due to the flat angle of glide, the aircraft touching down at {{convert|200|km/h|abbr=on}}. Once down safely, Brown and his much-relieved ground crew celebrated with a drink.<ref name="Wings on my Sleeve, p105-106" >Brown 2006, pp. 105–106.</ref><ref>{{cite web |url = https://www.heraldscotland.com/news/13713648.heroic-test-pilot-reunited-rocket-powered-messerschmitt/ |title = Heroic test pilot is reunited with rocket powered Messerschmitt |publisher = heraldscotland.com |first = John |last = Bynorth |date = 11 September 2015}}</ref>

Beyond Brown's unauthorised flight, the British never tested the Me 163 under power themselves; due to the danger of its [[hypergolic]] propellants it was only flown unpowered. Brown himself piloted RAE's Komet [[United Kingdom military aircraft serials|''VF241'']] on a number of occasions, the rocket motor being replaced with test instrumentation. When interviewed for a 1990s television programme, Brown said he had flown five tailless aircraft in his career (including the British [[de Havilland DH 108]]). Referring to the Komet, he said "this is the only one that had good flight characteristics"; he called the other four "killers".<ref>{{cite episode |title = Messerschmitt Me 163 Komet |series = Wings of the Luftwaffe |network = Discovery Military Channel |time = 44:09 (25:00 minutes) |language = en}}</ref>


==Surviving aircraft==
It has been claimed that at least 29 ''Komets'' were shipped out of Germany after the war and that of those at least 10 have been known to survive the war to be put on display in museums around the world.<ref>Ethell 1978, pp. 157–158.</ref> Most of the 10 surviving Me 163s were part of JG 400, and were captured by the British at [[Husum (Schleswig)|Husum]], the squadron's base at the time of Germany's surrender in 1945. According to the RAF museum, 48 aircraft were captured intact and 24 were shipped to the United Kingdom for evaluation, although only one, ''VF241'', was test flown (unpowered).<ref name="rafm">Simpson, Andrew. [https://www.rafmuseum.org.uk/documents/collections/85-AF-66-Me-163B.pdf "Individual History Messerschmitt ME163B-1a W/NR.191614/8481M"] {{webarchive|url=https://web.archive.org/web/20140201215155/http://www.rafmuseum.org.uk/documents/collections/85-AF-66-ME-163B-191614.pdf |date=1 February 2014}}. Royal Air Force Museum, 2007. Retrieved: 2 November 2009.</ref>

===Australia===
[[File:Me 163 191907 on display at the Australian War Memorial May 2015.jpg|thumb|Me 163B, Werknummer 191907, is part of the collection of the [[Australian War Memorial]] in Canberra]]

* Me 163B, Werknummer 191907 was part of JG 400, captured at Husum and was shipped to the RAE. It was allocated the RAF [[Air Ministry]] number of AM222 and was dispatched from Farnborough to No. 6 MU, [[RAF Brize Norton]], on 8 August 1945. On 21 March 1946, it was recorded in the Census of No. 6 MU, and allocated to No. 76 MU (Wroughton) on 30 April 1946 for shipment to Australia. For many years this aircraft was displayed at [[RAAF Williams]] Point Cook, but in 1986, the Me 163 was transferred to The [[Australian War Memorial]] for refurbishment. It was stored at the AWM Treloar Technology Annex Mitchell, refurbished and reassembled, and was later put up for display together with a [[Messerschmitt Me 262]]A-2a, Werknummer 500200 (AM81).<ref>Butler 1994, p. 107.</ref>

===Canada===
[[File:Me 163 Komet Displayed at the Canadian Aviation and Space Museum.jpg|thumb|right|Me 163B, Werknummer 191914, at the [[Canada Aviation and Space Museum]]; the tiny propeller operates as a [[ram air turbine]] that provides electrical power]]

* Me 163B, Werknummer 191659 (AM215) or 191914 (AM220), is held at the [[Canada Aviation and Space Museum]], Ottawa. Like two of the British Komets, this aircraft was part of JG 400 and captured at Husum. It was shipped to Canada in 1946.

: Werknummer 19116 (but more probable 191916) and 191095 (AM211) also seem to have been held at one time in this museum.<ref name="Pejčoch 2007, p. 69"/><ref>Ethell 1978, p. 158.</ref>

===Germany===
[[File:Me163.jpg|thumb|Messerschmitt Me 163 at the ''[[Luftwaffenmuseum]]'' in Berlin-Gatow]]

* A Me 163B, Werknummer 191904, "Yellow 25", belonging to JG 400 was captured by the RAF at Husum in 1945. It was sent to England, arriving first at Farnborough, receiving the RAF Air Ministry number AM219 and then transferred to [[RAF Brize Norton|Brize Norton]] on 8 August 1945, before finally being placed on display at the Station Museum at [[RAF Colerne|Colerne]]. When the museum closed in 1975 the aircraft went to [[RAF St Athan]], receiving the ground maintenance number 8480M. On 5 May 1988 the aircraft was returned to the [[Bundeswehr]]'s ''[[German Air Force|Luftwaffe]]'' air arm, and moved to the ''Luftwaffe'' [[Dassault-Breguet/Dornier Alpha Jet|Alpha Jet]] factory at the air base in Oldenburg (JBG 43), not far from the JG 400 unit's wartime base at [[Bad Zwischenahn]], now a golf course. The airframe was in good condition but the cockpit had been stripped and the rocket engine was missing.

Eventually an elderly German woman came forward with Me 163 instruments that her late husband had collected after the war, and the engine was reproduced by a machine shop owned by Me 163 enthusiast Reinhold Opitz. The factory closed in the early 1990s and "Yellow 25" was moved to a small museum created on the site. The museum contained aircraft that had once served as gate guards, monuments and other damaged aircraft previously located on the air base. In 1997 "Yellow 25" was moved to the official [[Luftwaffe Museum|''Luftwaffe'' Museum]] located at the former RAF base at [[Gatow Airport|Berlin-Gatow]], where it is displayed today alongside a restored Walter HWK 109–509 rocket engine. This particular Me 163B is one of the very few World War II–era German military aircraft, restored and preserved in a German aviation museum, to have a [[swastika]] marking, in a "low visibility" white outline form, currently displayed on the tailfin.

* Me 163B, Werknummer 120370, "Yellow 6" of JG 400, is displayed at the [[Deutsches Museum]], [[Munich]]. It was originally sent to Britain, where it had received the RAF Air Ministry number AM210. It was given to the Deutsches Museum by [[RAF Biggin Hill]] Station. Some claim this is ''191316'', but that is still at the London Science Museum.{{citation needed|date=March 2017}}

===United Kingdom===
Of the 21 aircraft that were captured by the British, at least three have survived. They were assigned the British [[United Kingdom military aircraft serials|serial numbers]] AM200 to AM220.<ref name="Pejčoch 2007, p. 69">Pejčoch 2007, p. 69.</ref>

* Me 163B, Werknummer 191316, "Yellow 6", has been on display at the [[Science Museum (London)|Science Museum]] in London, since 1964 with the Walter motor removed for separate display. A second Walter motor and a [[takeoff]] dolly are part of the museum's reserve collection and are not generally on display to the public.
* Me 163B, Werknummer 191614, is now displayed at the [[RAF Museum London]], where it was moved from the [[Royal Air Force Museum Midlands]] site at [[RAF Cosford]], its former home since 1975. Before then, it was at the [[Rocket Propulsion Establishment]] at Westcott, Buckinghamshire.<ref> RAF Museum Official Site[https://www.rafmuseum.org.uk/research/collections/messerschmitt-me-163b-1a-komet/"]</ref>
* Me 163B-1a, Werknummer 191659 and RAF [[Air Ministry]] serial number AM215, "Yellow 15", was captured at Husum in 1945 and was sent to the College of Aeronautics at [[Cranfield]], England in 1947. After many years of touring airshows and various outdoor gatherings around the UK it was loaned to the [[National Museum of Flight]] at [[East Fortune]] Airfield, [[East Lothian]], Scotland in 1976.

===United States===
[[File:Messerchmitt Me163B-2 (4976596499).jpg|thumb|Me 163B 191 301 at [[Wright Field]] display in October 1945]] 
[[File:Messerschmitt Me 163B-1a Komet.jpg|thumb|Unrestored Messerschmitt Me 163B ''Komet'' at the [[Udvar-Hazy center]]]]
[[File:Me 163B.jpg|thumb|Me 163B at [[Wright-Patterson National Air Force Museum]]]]

* Five Me 163s were originally brought to the United States in 1945, receiving the Foreign Equipment numbers FE-495 and FE-500 to 503.<ref>Andrade 1979, p. 251.</ref> An Me 163 B-1a, Werknummer (serial number) 191301, arrived at Freeman Field, Indiana, during mid-1945, and received the foreign equipment number FE-500. On 12 April 1946, it was flown aboard a cargo aircraft to the U.S. Army Air Forces facility at Muroc dry lake in California for flight testing. Testing began on 3 May 1946 in the presence of Dr. [[Alexander Lippisch]] and involved towing the unfueled ''Komet'' behind a [[Boeing B-29 Superfortress]] to an altitude of {{convert|9000|-|10500|m|ft|abbr=on}} before it was released for a glide back to earth under the control of test pilot Major Gus Lundquist.<ref>{{cite web |url = https://www.aerotechnews.com/blog/2022/03/21/high-desert-hangar-stories-a-tale-of-two-bobs-flight-test-legends-bob-cardenas-and-bob-hoover/ |title = High Desert Hangar Stories: A tale of two Bobs: Flight test legends Bob Cardenas and Bob Hoover |publisher = aerotechnews.com |first = Bob |last = Alvis |date = 21 March 2022}}</ref> Powered tests were planned, but not carried out after delamination of the aircraft's wooden wings was discovered. It was then stored at [[Norton AFB]], California until 1954, when it was transferred to the Smithsonian Institution. The aircraft remained on display in an unrestored condition at the museum's [[Paul E. Garber Preservation, Restoration, and Storage Facility]] in [[Suitland, Maryland]], until 1996, when it was lent to the [[Mighty Eighth Air Force Museum]] in [[Pooler, Georgia]] for restoration and display. It has since been returned to the Smithsonian and as of 2011 is on display unrestored at the National Air and Space Museum's [[Steven F. Udvar-Hazy Center]] near [[Washington D.C.]]
* Me 163B, Werknummer 191 095, is on fully restored display at the [[National Museum of the United States Air Force]] at [[Wright-Patterson AFB]] near [[Dayton, Ohio]]. It was acquired from the Canadian National Aviation Museum (now the [[Canada Aviation and Space Museum]]), where it had been restored, and was placed on display 10 December 1999. ''Komet'' test pilot {{ill|Rudolf Opitz (pilot)|lt=Rudolf "Rudi" Opitz|de|Rudolf Opitz (Pilot)}} was on hand for the dedication of the aircraft and discussed his experiences of flying the rocket-propelled fighter to a standing room only crowd. During the aircraft's restoration in Canada it was discovered that the aircraft had been assembled by French forced laborers who had deliberately sabotaged it by placing stones between the rocket's fuel tanks and its supporting straps. There are also indications that the wing was assembled with contaminated glue. Patriotic French writing was found inside the fuselage. The aircraft is displayed without any unit identification, but has its Werknummer restored<ref>{{cite web |url=https://media.defense.gov/2005/Dec/22/2000574802/-1/-1/0/030801-F-1234P-080.JPG |title=NMUSAF photo of WkNr. 191 095}}</ref> to its normal fin location. Fully restored examples of both the Me 163B's single-chamber rocket motor,<ref>{{cite web |url=https://www.nationalmuseum.af.mil/Visit/Museum-Exhibits/Fact-Sheets/Display/Article/196240/walter-hwk-509a-rocket/ |title=Walter HWK 509A Rocket |website=National Museum of the United States Air Force™}}</ref> as well as the only known example in the United States of the experimental twin-chamber Walter 509B rocket motor,<ref>{{cite web |url=https://www.nationalmuseum.af.mil/Visit/Museum-Exhibits/Fact-Sheets/Display/Article/196241/walter-hwk-509b-1-rocket/ |title=Walter HWK 509B-1 Rocket |website=National Museum of the United States Air Force™}}</ref> are each on display in front, one each to either side, of WkNr. 191 095.
[[File:1983 at Duxford Messerschmitt Me 163 191660.jpg|thumb|191660 placed alongside a B-17 at Duxford in 1983.]]
* Me 163B, Werknummer 191660, "Yellow 3", is owned by [[Paul Allen]]'s [[Flying Heritage Collection]]. Between 1961 and 1976, this aircraft was displayed at the [[Imperial War Museum]] in London. In 1976, it was moved to the [[Imperial War Museum Duxford]]. It underwent a lengthy restoration, beginning in 1997, that was frequently halted as the restorers were diverted to more pressing projects. In May 2005, it was sold, reportedly for £800,000, to raise money for the purchase of a [[De Havilland DH.9|de Havilland/Airco DH.9]] as the Duxford museum had no examples of a World War I bomber in its collection. Permission for export was granted by the British government's [[Department for Culture, Media and Sport]] as three other ''Komets'' were held in British museums.

==Japanese versions==
{{Main|Mitsubishi J8M}}

As part of their alliance, Germany provided the Japanese Empire with plans and an example of the Me 163.<ref>Ethell 1978, pp. 155–157.</ref> One of the two submarines carrying Me 163 parts did not arrive in Japan, so at the time, the Japanese lacked all of the major parts and construction blueprints, including the turbopump, which they could not make themselves, forcing them to reverse-engineer their own design from information obtained in the Me 163 Erection & Maintenance manual obtained from Germany. The prototype J8M crashed on its first powered flight and was completely destroyed,<ref>Späte 1989, p. 243.</ref> but several variants were built and flown, including: [[trainer (aircraft)|trainers]], [[fighter aircraft|fighters]], and [[interceptor aircraft|interceptors]], with only minor differences between the versions.

The Navy version, the [[Mitsubishi J8M]]1 ''Shūsui'', replaced the Ho 155 cannon with the Navy's 30&nbsp;mm (1.18&nbsp;in) [[Type 5 cannon]]. Mitsubishi also planned on producing a version of the 163C for the Navy, known as the J8M2 ''Shūsui'' Model 21. A version of the 163 D/263 was known as the J8M3 ''Shusui'' for the Navy with the Type 5 cannon, and a [[Rikugun Ki-202|Ki-202]] {{Nihongo|''Shūsui-kai''|秋水改||extra="Autumn Water, modified"}} with the Ho 155-II for the Army. Trainers were planned, roughly the equivalent of the Me 163 A-0/S; these were known as the [[Yokosuka MXY8|Kugisho/Yokosuka MXY8 (Yokoi Ki-13)]] {{Nihongo|''Akigusa''|秋草|extra="Autumn Grass"}} (an unpowered glider trainer) and [[Yokosuka MXY9|Kugisho/Yokosuka MXY9]] {{Nihongo|''Shūka''|秋花|extra="Autumn Flower"}} (a [[Ishikawajima Tsu-11|Tsu-11]]-powered [[motorjet]] trainer).

One complete example of the Japanese aircraft survives at the [[Planes of Fame Air Museum]] in the US. The fuselage of a second aircraft is displayed at the Mitsubishi company's Komaki Plant Museum, at [[Komaki, Aichi]] in Japan.<ref>[http://www.j-aircraft.com/misc/SURVIVE.HTM "List of surviving Japanese aircraft"] {{Webarchive|url=https://web.archive.org/web/20100125075927/http://www.j-aircraft.com/misc/SURVIVE.HTM |date=25 January 2010 }}. j-aircraft.com. Retrieved; 27 October 2010.</ref>

==Replicas==
[[File:Messerschmitt Me 163B-1a Komet, Private JP6586040.jpg|thumb|The Me 163 replica glider, ''D-1636'', Aérodrome de La Ferté-Alais, France, 2009]]
A flying replica Me 163 was constructed between 1994 and 1996 by Joseph Kurtz, a former ''Luftwaffe'' pilot who trained to fly Me 163s, but who never flew in combat. He subsequently sold the aircraft to [[EADS]]. The replica is an unpowered glider whose shape matches that of an Me 163, although its construction is completely different: the glider is built of wood with an empty weight of {{convert|285|kg|lb}}, a fraction of the weight of a wartime aircraft. Reportedly, it has excellent flying characteristics.<ref>de Bie, Rob. [https://robdebie.home.xs4all.nl/me163/kurz.htm "Mr Kurz' flying glider replica"]. Me 163 Komet Website, 10 July 2012. Retrieved: 27 May 2013.</ref> The glider is painted red to represent the Me 163 flown by [[Wolfgang Späte]]. It is not currently flown,<ref>{{Cite web |date=2018-03-29 |title=Aeroplane Datafile: Me 163 Komet |url=https://www.key.aero/article/aeroplane-datafile-me-163-komet |access-date=2024-10-29 |website=www.key.aero |language=en}}</ref> but is exhibited at the Messerschmitt Museum of Flight.<ref>{{Cite web |title=Messerschmitt Museum of Flight - Aircraft - Me 163 BS |url=https://www.flugmuseum-messerschmitt.com/AIRCRAFT-AND-CREW/Me-163-BS/index.php |access-date=2024-10-29 |website=www.flugmuseum-messerschmitt.com}}</ref>

In the early 2000s, a rocket-powered airworthy replica, the ''Komet II'', was proposed by [[XCOR Aerospace]], a former aerospace company that had previously built the [[XCOR EZ-Rocket]] rocket-plane. Although outwardly the same as a wartime aircraft, the ''Komet II''{{-'}}s design would have differed considerably for safety reasons. It would have been partially constructed with composite materials, powered by one of XCOR's own simpler and safer, pressure fed, liquid oxygen/alcohol engines, and retractable undercarriage would have been used instead of a takeoff dolly and landing skid.<ref>[https://web.archive.org/web/20031003124607/http://www.xcor.com/me163.html "Me 163 Flying Replica"]. Internet Archive, 1 October 2003. Retrieved: 26 December 2008.</ref>

Several static replica Me 163s are exhibited in museums.{{citation needed|date=March 2017}}

==Specifications: Me 163B-1a==
[[File:Messerschmitt Me 163 3-view.svg|thumb|Messerschmitt Me 163B 3-view drawings]]
{{Aircraft specs
|ref= ''The Warplanes of the Third Reich'',<ref name=Green>{{cite book |last1 = Green |first1 = William |last2 = Punnett |first2 = Dennis (With line drawings by) |title = The Warplanes of the Third Reich |date = 1970 |publisher = Doubleday |location = Garden City, N.Y. |isbn = 0385057822 |pages = 594–606}}</ref> ''Profile No225: Messerschmitt Me 163 Komet''<ref name="Bateson">{{cite journal |last1 = Bateson |first1 = Richard P. |last2 = Spate |first2 = Wolfgang |title = Messerschmitt Me 163 Komet |journal = Aircraft in Profile |date = 1971 |issue = 225}}</ref>
|prime units?= met
<!--
General characteristics
-->
|crew= 1
|capacity= (Me 163S + 1)
|length m= 5.7
|span m= 9.3
|height m= 2.5
|wing area sqm= 19.6
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight lb= 4,200
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight lb= 9,500
|fuel capacity=<br/>
** '''''[[C-Stoff]]''''' (fuel) {{cvt|468|kg}}
** '''''[[T-Stoff]]''''' (oxidizer) {{cvt|1550|kg}}
|more general=
<!--
Powerplant
-->
[[File:Plan view of a Messerschmitt Me 163 Komet.jpg|thumb|Plan view of the un-restored Messerschmitt Me 163 Komet at the Smithsonian Institute's Udvar-Hazy Center in Chantilly, Virginia, USA.]]
|eng1 number= 1
|eng1 name= [[Hellmuth Walter Kommanditgesellschaft]] [[HWK 109-509A-2]]
|eng1 type= bi-propellant liquid-fuelled rocket motor
|eng1 lbf= 3,307
|eng1 note= maximum; {{cvt|220|lbf|order=flip}} minimum, fully variable
<!--
Performance
-->
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh= 900
|never exceed speed note= at all altitudes, sea level to {{cvt|12000|m}}{{clarify|The often quoted top speed of {{convert|596|mi/h|km/h|abbr=on}} up to the tropopause is impossible, as it corresponds to a Mach Number of over .89—the Me 163B ran into severe compressibility above .82 and complete loss of control at M=.84. This anomaly has not been explained, although it might relate to uncompensated instrumentation on the operational aircraft.|date=December 2017}}<br/>
* '''Flap limiting speed:''' {{cvt|300|km/h|mph kn}}
* '''Rotate speed at take-off:''' {{cvt|280|km/h|mph kn}}
* '''Best climbing speed:''' {{cvt|700|-|720|km/h|mph kn}}
|endurance= 7.5 mins powered
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin= 16,000
|time to altitude= From standing start<br/>
** {{cvt|2000|m}} in 1.48 min
** {{cvt|4000|m}} in 2.02 min
** {{cvt|6000|m}} in 2.27 min
** {{cvt|8000|m}} in 2.54 min
** {{cvt|10000|m}} in 3.19 min
** {{cvt|12000|m}} in 3.45 min
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2= 209
|wing loading note= at maximum take-off weight
|fuel consumption kg/km=
|fuel consumption lb/mi=
|thrust/weight= 0.42
|more performance=
<!--
Armament
-->
|guns=<br/>
** 2 × {{cvt|30|mm|3}} Rheinmetall Borsig [[MK 108 cannon]] with 60 rpg

}}

==See also==
{{Portal|Aviation}}
* [[Hanna Reitsch]]
{{aircontent|
|related=
* [[Lippisch Delta IV|DFS-39]]
* [[DFS-194]]
* [[Messerschmitt Me 263]]
* [[Mikoyan-Gurevich I-270]]
* [[Mitsubishi J8M]]
|similar aircraft=
* [[Bachem Ba 349]]
* [[Bereznyak-Isayev BI-1]]
* [[Focke-Wulf Volksjäger]]
|lists=
* [[List of aircraft of World War II]]
* [[List of military aircraft of Germany]]
* [[List of fighter aircraft]]
* [[List of rocket-powered aircraft]]
* [[List of World War II military aircraft of Germany]]
* [[Wunderwaffe]]
}}

==References==
===Notes===
{{Reflist|group=N}}

===Citations===
{{Reflist}}

===Bibliography===
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* {{cite book |last1 = Späte |first1 = Wolfgang |title = Top Secret Bird: Luftwaffe's Me-163 Komet |location = Missoula, Montana, US |publisher = Pictorial Histories Publishing Co. |date = 1989 |isbn = 1-872836-10-0}}
* {{cite book |last1 = Späte |first1 = Wolfgang |first2 = Richard P. |last2 = Bateson |title = Messerschmitt Me 163 Komet (Aircraft in Profile number 225) |location = Windsor, Berkshire, UK |publisher = Profile Publications Ltd. |date = 1971}}
* {{cite book |last1 = Spick |first1 = Mike |title = Aces of the Reich: The Making of a Luftwaffe Fighter-Pilot |date = 2006 |publisher = Greenhill Books |isbn = 9781853676758}}
	
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* {{cite book |last1 = Stüwe |first1 = Botho |title = Peenemünde West |language = German |location = Augsburg, Germany |publisher = Bechtermünz Verlag |date = 1999 |isbn = 3-8289-0294-4}}
* {{cite book |last1 = Thompson |first1 = J. Steve |first2 = Peter C. |last2 = Smith |title = Air Combat Manoeuvres: The Technique and History of Air Fighting for Flight Simulation |location = Hersham, Surrey, UK |publisher = Ian Allan Publishing |date = 2008 |isbn = 978-1-903223-98-7}}
* {{cite book |last1 = Volmar |first1 = Joe |title = I Learned to Fly for Hitler |date = 1999 |publisher = Kron Publications |location = Dundee |isbn = 9780967138909 }}
* {{cite book |last1 = Walker |first1 = Bryce |title = Fighting jets |date = 1983 |publisher = Time-Life Books |location = Alexandria, Va. |edition = 1 |isbn = 0-8094-3362-1}}
* {{cite book |last1 = Wilson |first1 = Stewart |title = Aircraft of WWII |location = Fyshwick, ACT, Australia |publisher = Aerospace Publications Pty Ltd |date = 1998 |isbn = 1-875671-35-8}}
* {{cite magazine |last = Yamakazi |first = Akio |title = Tail of the Tiger |magazine = [[Air Enthusiast]] |date = January–February 2005 |issue = 115 |pages = 36–41 |issn = 0143-5450}} 
* {{cite book |last1 = Ziegler |first1 = Mano |title = Rocket Fighter: The Story of the Messerschmitt Me 163 |location = London, UK |publisher = Arms and Armour Press |date = 1976 |isbn = 0-85368-161-9}}

==External links==
{{Commons category}}
* [https://books.google.com/books?id=PyEDAAAAMBAJ&dq=motor+gun+boat&pg=PA83 "Fastest Controlled Flight"], October 1944, ''[[Popular Science]]''. Earliest drawing released by USAAF to public about Me 163
* [https://books.google.com/books?id=xiADAAAAMBAJ&dq=popular+science+%22A+two-room+wing%22&pg=PA124 "Secrets of the German Jet Planes"]. June 1945, ''[[Popular Science]]'' page 124—the first detailed drawing in a general public magazine
* [https://www.youtube.com/watch?v=TBXyoInJC1M 8th Airforce engages Me 163s in air to air combat]

{{Messerschmitt aircraft}}
{{RLM aircraft designations}}
{{Lippisch aircraft}}
{{Authority control}}

[[Category:Messerschmitt aircraft|Me 163]]
[[Category:German inventions]]
[[Category:High-test peroxide]]
[[Category:Rocket-powered aircraft]]
[[Category:Tailless aircraft]]
[[Category:1940s German fighter aircraft]]
[[Category:1941 in Germany]]
[[Category:1941 in science]]
[[Category:Aircraft first flown in 1941]]
[[Category:Mid-wing aircraft]]
[[Category:Aircraft with skid landing gear]]