View source for Luna 4

{{Short description|Space probe}}
{{Use mdy dates|date=May 2020}}
{{italic title}}
{{Infobox spaceflight
| name                  = ''Luna 4''
| image                 = Luna 9 Musee du Bourget P1010505.JPG
| image_size            = 
| image_caption         = Mockup of the Luna 9 (a Ye-6 series), Museum of Air and Space Paris, Le Bourget (France)

| mission_type          = [[Moon|Lunar]] lander
| operator              = Soviet space program
| COSPAR_ID             = 1963-008B<ref name=nssdc>{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1963-008B|title=Luna 4|website=NASA Space Science Data Coordinated Archive|access-date=25 August 2024}}{{PD-notice}}</ref>
| SATCAT                = 566<ref name=nssdc />
| mission_duration      = 13 days (launch to last contact)
| spacecraft            = [[Luna_programme#Soft_landers|Ye-6]] No.4<ref name=gunter>{{cite web|url=https://space.skyrocket.de/doc_sdat/luna_e6.htm|title=Luna Ye-6|website=Gunter's Space Page|last1=Krebs|first1=Gunter|access-date=October 22, 2019}}</ref>
| spacecraft_type       = 
| manufacturer          = [[OKB-1]]
| dry_mass              = 
| launch_mass           = {{convert|1422|kg}}
| power                 =
| launch_date           = {{start-date|April 2, 1963, 08:04:00|timezone=yes}}&nbsp;UTC<ref name=nssdc />
| launch_rocket         = [[Molniya-L]] 8K78/E6
| launch_site           = [[Baikonur Cosmodrome|Baikonur]] [[Baikonur Cosmodrome Site 1|1/5]]<ref name=gunter />
| launch_contractor     = 
| last_contact          = April 15, 1963
| orbit_epoch           = April 2, 1963<ref name=nssdc/> 
| orbit_reference       = 
| orbit_periapsis       = {{cvt|690000|km}}<ref name=nssdc/> 
| orbit_apoapsis        = {{cvt|89250|km}}<ref name=nssdc/> 
| orbit_inclination     = 
| orbit_period          = 
| orbit_semimajor       = 
| orbit_eccentricity    = 
| apsis                 = apsis
| programme             = '''[[Luna programme]]'''
| previous_mission      = ''[[Luna E-6 No.3|Luna 1963B]]''
| next_mission          = ''[[Luna E-6 No.6|Luna 1964A]]''
|interplanetary         = 
 {{Infobox spaceflight/IP
   |type                = lander_flyby
   |object              = [[Moon|Lunar]]
   |arrival_date        =  April 5, 1963, 13:25 UT
   |distance            = {{convert|8400|km}}
 }}
}}
'''''Luna 4''''', or '''E-6 No.4''' (Ye-6 series), sometimes known in the West as '''Lunik 4''', was a [[Soviet Union|Soviet]] spacecraft launched in 1963 as part of the [[Luna program]] to attempt the first [[soft landing (rocketry)|soft landing]] on the [[Moon]]. Following a successful launch, the spacecraft failed to perform a course correction and as a result it missed the Moon, remaining instead in Earth orbit before possibly transitioning into a solar orbit. Though the mission was unsuccessful, it nevertheless marked a new epoch in the [[Space Race]], which culminated in the successful landing of [[Luna 9]] in 1966.

==Background==

On the heels of the successful [[Luna 3]] mission, which returned the first images of the Far Side of the Moon, the Soviet Union turned its attention to learning more about the lunar surface and whether it was solid enough to land and build structures upon. To this end, on 10 December 1959, Soviet Premier [[Nikita Khrushchev]] signed a resolution of the Central Committee and Council of Ministers for the creation of a lunar soft lander equipped with scientific instrumentation and a television. This task was assigned to a group led by Nikolay Beresnev, working in the section of [[Mikhail Tikhonravov]]'s department at [[OKB-1]] run by Gleb Maksimov. OKB-1 chief [[Sergei Korolev]] took a personal hand in leading the project initially before handing the reins to Beresnev.<ref name=ranp3>{{cite book|author=Boris Chertok|title=Rockets and People, Volume III: Hot Days of the Cold War|publisher=NASA|location=Washington D.C.|date=June 2009|oclc=656365714}}</ref>{{rp|376-377}} By 1963, de facto management of the project had devolved onto [[Boris Chertok]].<ref name=ranp3/>{{rp|381}} The working designation was Ye-6 ("Ye" being the letter in the alphabet succeeding "D", the designation given to the satellite project that became [[Sputnik 3]]).<ref name=ranp3>{{cite book|author=Boris Chertok|title=Rockets and People, Volume III: Hot Days of the Cold War|publisher=NASA|location=Washington D.C.|date=June 2009|oclc=656365714}}</ref>{{rp|377ff}}

Because of the complexity of the Ye-6 spacecraft, its mass was too great for the three-stage [[Luna (rocket)]] that had launched the previous Luna probes. The Ye-6 instead would be launched on the 8K78 booster which allowed a larger payload and provided the ability to put the probe in a parking orbit rather than the inaccurate direct ascent of the first generation Luna probes, although of the first ten 8K78 launch attempts, only two ([[Mars 1]] and [[Venera 1]]) succeeded, the rest failing to reach orbit or being unable to leave LEO.<ref name=ranp3/>{{rp|379}} Combined with the advanced nature of the lander, the Ye-6 team estimated that the mission had a 10% chance of success.<ref name=ranp3/>{{rp|381}}

==Spacecraft==

The Ye-6 spacecraft consisted of a stack of three cylindrical modules, with a height of {{cvt|2.7|m}} and a launch mass of {{cvt|1422|kg}}. The first module was the Isayev rocket module, which held the main engine, used for mid-course correction and the descent to landing, four thrusters for attitude control, and two cruise modules. The main engine propellant was [[hypergolic]], consisting of [[nitric acid]] and [[amine]] and producing a thrust of about 45,000 [[Newton (unit)|N]]. The four thrusters were mounted on outriggers and could produce 245 N each. A {{cvt|5|m}} boom would be deployed from the bottom of the spacecraft, used to trigger the final landing sequence. The second module was a hermetically sealed pressurized compartment that held the propellant and oxygen and contained communication, attitude orientation, an altimeter, and the onboard control system ("I-100").<ref name=nssdc/>

Luna 4 carried an astronavigation system so that it could autonomously change course midflight. This device (SAN) was derived from similar systems developed for aircraft. The spacecraft's autonomous control system, gyroscopes, control and logic circuits were all combined in the {{cvt|80|kg}} I-100 package that also controlled aspects of the Molniya rocket's third and fourth stages; this was a weight-saving measure that, nevertheless, was conducive to failures, as had occurred when similar solutions had been applied to the [[Mars program|Mars]] and [[Venera]] spacecraft.<ref name=ranp3/>{{rp|379}}

The third module was the lunar lander, a {{cvt|58|cm}} diameter sphere protected by two hemispherical airbags. The {{cvt|105|kg}} sphere had a hermetically sealed compartment that held communications apparatus, batteries, thermal control systems, a timer, and the science experiments. The top of the sphere had four petals, which would open up on landing, allowing deployment of four {{cvt|75|cm}} whip antennas and the lander camera turret. Control of the lander was done by the timing device onboard or by communication from Earth. The batteries were designed to operate for a total of 5 hours over about 4 days.<ref name=nssdc/> 

The scientific payload comprised an imaging system and an SBM-10 radiation detector.<ref name=nssdc/> The latter was a [[Geiger counter|gas-discharge counter]], {{cvt|50|mm}} long and {{cvt|10|mm}} in diameter, heavily shielded on one side. Radiation counts were telemetered continuously with a statistical accuracy of about 0.1%.<ref name=study>{{cite journal|author1=S. N. Vernov |author2=A. Ye. Chudakov |author3=P. V. Vakulov |author4=Ye. V. Gorchakov |author5=Yu. I. Logachev |author6=G. P. Lyubimov |author7=A. G. Nikolayev|title=Investigation of Radiation with the Flights of the "Mars 1" and "Luna 4" Interplanetary Automatic Stations|journal=Cosmic Research |volume= 2 |issue= 4 |year=1964 |language= Russian|url=https://apps.dtic.mil/dtic/tr/fulltext/u2/605513.pdf|archive-url=https://web.archive.org/web/20190426223255/https://apps.dtic.mil/dtic/tr/fulltext/u2/605513.pdf |archive-date=April 26, 2019 }}</ref>

The mission plan was to initialize the landing sequence at an altitude of about {{cvt|8300|km}}. At {{cvt|70|km}} to {{cvt|75|km}} altitude the cruise modules would be jettisoned, the main engine would start, the radar altimeter would be activated, and the lander airbags would inflate. At {{cvt|250|m}} to {{cvt|265|m}} altitude the main engine would shut off and the four thrusters would ignite. The {{cvt|5|km}} meter boom would touch the surface first, causing the ejection of the lander, which would hit the surface, cushioned by the airbags, at about {{cvt|15|m/s}}. The airbags would deflate, the petals would open, causing the sphere to be oriented correctly, and the antennas and instruments could be deployed.<ref name=nssdc/>{{PD-notice}}

==Mission==


After a development process fraught with technical and jurisdictional delays, the first flight version of the Ye-6 was built in December 1962. Launches on 4 January 1963 ([[Luna E-6 No.2]]) and 3 February 1963 ([[Luna E-6 No.3]]) failed--one was stuck in LEO and another failed to reach orbit.<ref name=ranp3/>{{rp|382-383}}

Luna 4 was launched by a [[Molniya-L]] carrier rocket at 08:16:37 UTC on April 2, 1963. Launch occurred from [[Baikonur Cosmodrome Site 1|Site 1/5]] at the [[Baikonur Cosmodrome]],<ref name=gunter /><ref name=log>{{Cite web|url=https://planet4589.org/space/gcat/data/derived/launchlog.html|title=Launch Log|last=McDowell|first=Jonathan|publisher=Jonathon's Space Report|access-date=25 August 2024}}</ref> and the mission was tracked and controlled from [[Simferopol]], including the {{convert|32|m}} parabolic antenna sited there.<ref name=ranp3/>{{rp|385}} After reaching an initial parking orbit of {{convert|167|by|182|km|mi}}, the rocket's upper stage restarted to place Luna 4 onto a translunar trajectory.<ref name=nssdc/>

Luna 4's initial trajectory was according to plan, but due to a failure of the Yupiter astronavigation system, most likely due to thermal control problems, the spacecraft could not be oriented properly for the planned midcourse correction burn. As a result, Luna 4 missed the Moon by about {{convert|8400|km}} at 13:25 UT on April 5, 1963. It then entered a [[Barycentric coordinates (astronomy)|barycentric]] {{cvt|90000|km}} × {{cvt|700000|km}} Earth orbit.<ref name=nssdc/> 

Although coverage of the flight was front page news outside of the USSR, details released by [[TASS]], the Soviet news agency, were scant.<ref name=timesadvocate>{{cite news|newspaper=Escondido Times-Advocate|date=3 April 1963|title=Russian Moon-Rocket Reaches Half-Way Mark|page=1|url=https://www.newspapers.com/image/568039291/|url-access=subscription}}</ref> This irritated Chertok and his team, who felt the secrecy "belittle[d] the real significance of the space program and generate[d] doubt among the public as to its practicality."<ref name=ranp3/>{{rp|385}}

Despite (and in some ways because of) the relative lack of information, Western scientists were able to deduce much about the Luna 4 (known as "Lunik 4") mission. For instance, logic dictated that the next step after the prior lunar missions would be either a lunar orbiter or a soft-lander. The comparatively long mission length of 3.5 days implied a larger payload, supporting this belief. That Luna 4 missed the Moon, and by a wider margin than [[Luna 1]] and [[Luna 3]], thus suggested a mission failure.<ref name=avweek1963b>{{cite magazine|date=15 April 1963|title=Lunik 4 Believed to Have Failed in Mission|url=http://archive.aviationweek.com/issue/19630415#!&pid=38|magazine=Aviation Week and Space Technology|publisher=McGraw Hill Publishing Company|access-date=23 August 2024|page=38|url-access=subscription}}</ref>

Additional evidence was provided by Radio Moscow's virtual silence regarding the flight as well as the cancellation of the television program "Hitting the Moon", scheduled for 7:45pm Moscow time on April 5, coinciding with Luna 4's arrival at the Moon. A poetry program and a piano interlude were played instead. TASS reports on the probe were uncharacteristically brief, and the last mention of the probe in the newspaper [[Pravda]] was a short reference within a general article on the Moon, which was published April 7.<ref name=avweek1963b/>

==Results and status==

The spacecraft transmitted at 183.6 [[Hertz|MHz]] until 15 April.<ref name=rsp>{{cite book|title=Russian Space Probes: Scientific Discoveries and Future Missions|author1=Brian Harvey|author2=Olga Zakutnyaya|date=2011|publisher=Springer Praxis Books|pages=166–167|location=Chichester,UK|oclc=1316077842}}</ref> French and Italian astronomers reported reception of pictures of the Moon taken by Luna 4. A {{convert|2.6|m}} telescope in Russia photographed Luna 4 early in its flight when it appeared as a 14th magnitude object.<ref name=avweek1963b/> Though Luna 4 did not land on the Moon, it did return data on the radiation environment in [[cislunar space]]. The spacecraft reported variations in the radiation flux over time comparable to those measured by previous missions, but with smoother transition times. Because Luna 4, unlike its predecessors, was launched during the [[solar minimum|least active part of the solar 11 year cycle]], it was conjectured that, rather than being caused by sporadic solar outbursts, that the more gentle variations detected by Luna 4 might instead be caused by changes in local magnetic field effects—normally undetectable in more active times.<ref name=study/> Luna 4 also discovered that the Earth's [[Magnetosphere#Magnetotail|geomagnetic tail]] seeped out at least as far as lunar orbit.<ref name=rsp/>

Luna 4's path appears to have been perturbed such that it now orbits the Sun rather than the Earth.<ref name=nssdc/> The Ye-6 program was ultimately successful, with the 12th in the series, [[Luna 9]], landing on the Moon on 3 February 1966.<ref name=ranp3/>{{rp|373}}

==See also==

* [[List of missions to the Moon]]

==References==
{{Reflist}}

==External links==
{{Portal|Spaceflight}}

{{Luna programme}}
{{Moon spacecraft}}
{{Orbital launches in 1963}}

[[Category:Luna programme|Luna 04]]
[[Category:Spacecraft launched in 1963]]
[[Category:1963 in the Soviet Union]]