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Image:RT-2.jpg 100px The RT-2 missile was the first intercontinental solid-propellant missile. Its first launch took place on February 26, 1966. In 1968 the missile was added to inventory. Category:Launch Vehicle

Image:RT-1launch.jpg 300px RT-1 missile The first strategic solid-propellant missile. Its first launch took place on April 28, 1962. Category:Launch Vehicle

... Infobox Spacecraft Name = '''''STS-2'''''
Image = Image:sts-2.jpg 200px Organization = NASA-Office of Space Flight (United States), NASA-Office of Space Science Applications ( ... experiments; Orbiter Experiments (OEX) Mission patch: Image:sts-2-patch.jpg 200px Books about the Space Shuttle Program Image:9781926837130.jpg '''Buy This Book''' http://www.apogeeprime.com/prime/bookpages ...

... MIR-2 space station''' Image:MIR2_Variant_0_English.jpg '''Variant 0 of MIR-2 space station''' Image:Variants_of_Payload_Modules_MIR2.jpg '''Variant of Payload Modules for MIR-2 space station''' Image:Mir-2.jpg '''Final version of the proposed permanently operating Mir-2 ...

Image:ISSELC.jpg 800 px Image:ISSELC-2.jpg Image:ISSELC-2a.jpg Category:International Space Station

Image:Venera2.jpg 300px Venera II probe in museum Image:Venera2-2.jpg 300px Venera-2 3MV-4 No. 4. Category:Spacecraft

Image:OR-2.jpg 300px The OR-2 liquid fuel engine designed by Fridrikh Zander . The OR-2 had a thrust of 50kg. It was designed for the RP-1 tailless glider designed by B.I. Cheranovsky in 1933. It was one of the first engines in Soviet Russia and was cooled with water and gaseous oxygen and burned oxygen and gasoline. Category:Rocket Engine

... became aware of the mechanics of our solar system. ref 4 Image:Glasgow_Observatory.jpg thumb Glasgow University Observatory ca. 1841 His friends at Glasgow included landscape painter ... 11 '''Part 11''' Footnotes note 1 ''The Presbyterian Historical Almanac'', 1864 note 2 ''The Journal of Education for Lower Canada'', Eighth Volume, 1864 note ...

Image:R-2rocket.jpg R-2 rocket schematic Image:R-2engineering.jpg R-2 engineering facilities Image:R-2launchfacility.jpg R-2 launch facilities Image:R-2launch.jpg R-2 launch Category:Launch Vehicle

... Of the initial weight of 1.6 million pounds in Earth orbit, approximately 1.2 million, or nearly 75%, are propellant. EN ROUTE SPACECRAFT CONFIGURATION The forward compartment ... capabilities for the longer periods required for the Manned Mars Landing Mission. Image:MMLVB11.jpg 300px '''En Route Spacecraft configuration artificial gravity mode''' The option to provide artificial ...

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