<?xml version="1.0"?>
<feed xmlns="http://www.w3.org/2005/Atom" xml:lang="en">
	<id>https://wiki.sarg.dev/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=98.38.82.170</id>
	<title>Vero - Wikipedia - User contributions [en]</title>
	<link rel="self" type="application/atom+xml" href="https://wiki.sarg.dev/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=98.38.82.170"/>
	<link rel="alternate" type="text/html" href="https://wiki.sarg.dev/index.php/Special:Contributions/98.38.82.170"/>
	<updated>2026-08-14T20:30:31Z</updated>
	<subtitle>User contributions</subtitle>
	<generator>MediaWiki 1.44.2</generator>
	<entry>
		<id>https://wiki.sarg.dev/index.php?title=Astrobee&amp;diff=810931</id>
		<title>Astrobee</title>
		<link rel="alternate" type="text/html" href="https://wiki.sarg.dev/index.php?title=Astrobee&amp;diff=810931"/>
		<updated>2025-08-28T04:38:57Z</updated>

		<summary type="html">&lt;p&gt;98.38.82.170: /* Astrobee 1500 */Fixed two places with Astrobe instead of Astrobee.&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{for|the space robot|Astrobee (robot)}}&lt;br /&gt;
&#039;&#039;&#039;Astrobee&#039;&#039;&#039; is the designation of series of American [[sounding rocket]]s with one to three stages.&amp;lt;ref name=&amp;quot;:0&amp;quot;&amp;gt;{{Cite web |title=Astrobee |url=http://astronautix.com/a/astrobee.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;:1&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:2&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:3&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:4&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:5&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:6&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:7&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:8&amp;quot; /&amp;gt;&amp;lt;ref&amp;gt;{{Cite web |title=Aerojet General Astrobee |url=https://www.designation-systems.net/dusrm/app4/astrobee.html |access-date=2023-10-18 |website=www.designation-systems.net}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Designed by [[Aerojet]], this family of [[Solid-propellant rocket|solid-propellant]] rockets was conceived as a lower-cost replacement of the liquid-propellant [[Aerobee]].&amp;lt;ref name=&amp;quot;:0&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:1&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:2&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:3&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:4&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:5&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:6&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:7&amp;quot; /&amp;gt;&amp;lt;ref name=&amp;quot;:8&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Versions ==&lt;br /&gt;
&lt;br /&gt;
=== Astrobee 500 ===&lt;br /&gt;
The three-stage &#039;&#039;&#039;Astrobee 500&#039;&#039;&#039; (first stage: &#039;&#039;Genius&#039;&#039;, second stage: &#039;&#039;[[Alcor (rocket engine)|Alcor]]&#039;&#039;, third stage: [[Asp (rocket)|&#039;&#039;Asp&#039;&#039;]]) has a ceiling of 1000&amp;amp;nbsp;km, a [[takeoff]] [[thrust]] of 161&amp;amp;nbsp;kN, a takeoff [[weight]] of 900&amp;amp;nbsp;kg, a [[diameter]] of 0.38 m and a length of 7.80 m.&amp;lt;ref name=&amp;quot;:1&amp;quot;&amp;gt;{{Cite web |title=Astrobee 500 |url=http://astronautix.com/a/astrobee500.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;:2&amp;quot;&amp;gt;{{Cite web |title=Astrobee-500 |url=https://space.skyrocket.de/doc_lau/astrobee-500.htm |access-date=2023-10-18 |website=Gunter&#039;s Space Page |language=en}}&amp;lt;/ref&amp;gt; It was launched one time in 1960.&amp;lt;ref name=&amp;quot;:2&amp;quot; /&amp;gt;&amp;lt;gallery&amp;gt;&lt;br /&gt;
File:Astrobee-500.jpg|Astrobee-500&lt;br /&gt;
&amp;lt;/gallery&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Astrobee 1500 ===&lt;br /&gt;
The three-stage &#039;&#039;&#039;Astrobee 1500&#039;&#039;&#039; (first stage: &#039;&#039;Recruit&#039;&#039;, second stage: &#039;&#039;Aero jet&#039;&#039;, third stage: &#039;&#039;Alcor&#039;&#039;) has a ceiling of 1000&amp;amp;nbsp;km, a takeoff thrust of 566&amp;amp;nbsp;kN, a takeoff weight of 5200&amp;amp;nbsp;kg, a diameter of 0.79 m and a length of 10.40 m.&amp;lt;ref name=&amp;quot;:3&amp;quot;&amp;gt;{{Cite web |title=Astrobee 1500 |url=http://astronautix.com/a/astrobee1500.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt; It was launched ten times between 1961 and 1969.&amp;lt;ref name=&amp;quot;:3&amp;quot; /&amp;gt;&amp;lt;gallery&amp;gt;&lt;br /&gt;
File:Astrobee-1500 - 1.jpg|Astrobee 1500&lt;br /&gt;
File:Astrobee-1500 2.jpg|Astrobee 1500&lt;br /&gt;
File:Astrobee 1500 first flight test, 21 October 1964.jpg|Astrobee 1500&lt;br /&gt;
&amp;lt;/gallery&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Astrobee 200 ===&lt;br /&gt;
The two-stage &#039;&#039;&#039;Astrobee 200&#039;&#039;&#039; (first stage: &#039;&#039;[[Nike (rocket stage)|Nike]]&#039;&#039;, second stage: &#039;&#039;Alcor&#039;&#039;),&amp;lt;ref&amp;gt;{{Cite web |title=Astrobee-200 |url=https://space.skyrocket.de/doc_lau_det/astrobee-200.htm |access-date=2025-01-19 |website=Gunter&#039;s Space Page |language=en}}&amp;lt;/ref&amp;gt; has a ceiling of 350&amp;amp;nbsp;km, a takeoff thrust of 161&amp;amp;nbsp;kN, a takeoff weight of 800&amp;amp;nbsp;kg, a diameter of 0.38 m and a length of 6.30 m. It was launched ten times between 1961 and 1966&amp;lt;ref name=&amp;quot;:4&amp;quot;&amp;gt;{{Cite web |title=Astrobee 200 |url=http://astronautix.com/a/astrobee200.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt;&amp;lt;gallery&amp;gt;&lt;br /&gt;
File:Astrobee-200.jpg|Astrobee 200&lt;br /&gt;
&amp;lt;/gallery&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Astrobee D ===&lt;br /&gt;
The single-stage &#039;&#039;&#039;Astrobee D&#039;&#039;&#039; has a ceiling of 140&amp;amp;nbsp;km, a takeoff thrust of 23.00&amp;amp;nbsp;kN, a takeoff weight of 100&amp;amp;nbsp;kg, a diameter of 0.15 m and a length of 3.90 m.&amp;lt;ref name=&amp;quot;:5&amp;quot;&amp;gt;{{Cite web |title=Astrobee D |url=http://astronautix.com/a/astrobeed.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;:6&amp;quot;&amp;gt;{{Cite web |title=Astrobee-D |url=https://space.skyrocket.de/doc_lau/astrobee-d.htm |access-date=2023-10-18 |website=Gunter&#039;s Space Page |language=en}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{Cite book |last=Bollermann |first=B. |url=https://ntrs.nasa.gov/citations/19710017216 |title=Study of 30 km to 200 km meteorological rocket sounding systems. |date=May 1, 1971 |publisher=NASA  |volume=2 - Recent advancements |pages=104–105 |chapter=Astrobee D |id=NASA-CR-1790}}&amp;lt;/ref&amp;gt; It was launched forty-two times between 1970 and 1980.&amp;lt;ref name=&amp;quot;:6&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Astrobee F ===&lt;br /&gt;
The single-stage &#039;&#039;&#039;Astrobee F&#039;&#039;&#039; has a ceiling of 375&amp;amp;nbsp;km, a takeoff thrust of 178.00&amp;amp;nbsp;kN, a takeoff weight of 1500&amp;amp;nbsp;kg, a diameter of 0.38 m and a length of 11.50 m.&amp;lt;ref name=&amp;quot;:7&amp;quot;&amp;gt;{{Cite web |title=Astrobee F |url=http://astronautix.com/a/astrobeef.html |access-date=2023-10-18 |website=astronautix.com}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;:8&amp;quot;&amp;gt;{{Cite web |title=Astrobee-F |url=https://space.skyrocket.de/doc_lau/astrobee-f.htm |access-date=2023-10-18 |website=Gunter&#039;s Space Page |language=en}}&amp;lt;/ref&amp;gt; It was launched forty-nine times between 1972 and 1983.&amp;lt;ref name=&amp;quot;:8&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{{commons category|Astrobee}}&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{Reflist}}&lt;br /&gt;
{{Suborbital_rocket_engines}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Sounding rockets of the United States]]&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
{{rocket-stub}}&lt;/div&gt;</summary>
		<author><name>98.38.82.170</name></author>
	</entry>
</feed>