remaining propellant

  • 1Rocket propellant — is mass that is stored, usually in some form of propellant tank, prior to being used as the propulsive mass that is ejected from a rocket engine in the form of a fluid jet to produce thrust.Chemical rocket propellants are most commonly used,… …

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  • 2Metal Storm — Metalstorm redirects here. For other uses, see Metal Storm (disambiguation). Metal Storm Limited Type Public (ASX: MST) …

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  • 3Saturn V — Infobox rocket caption = The first Saturn V, AS 501, before the launch of Apollo 4 name = Saturn V function = Manned LEO and Lunar launch vehicle manufacturer = Boeing (S IC) North American (S II) Douglas (S IVB) country origin = United States… …

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  • 4Rocket — This article is about vehicles powered by rocket engines. For other uses, see Rocket (disambiguation). A Soyuz U, at Baikonur Site 1/5 A rocket is a missile, spacecraft, aircraft or other vehicle which obtains thrust from a rocket engi …

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  • 5DIRECT — For other uses, see Direct (disambiguation). For the rockets proposed as part of the DIRECT architecture, see Jupiter (rocket family). DIRECT is a proposed alternative heavy lift launch vehicle architecture supporting NASA s Vision for Space… …

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  • 6Apollo 12 — Infobox Space mission mission name = Apollo 12 insignia = AP12goodship.png command module = CM 108 nowrap|callsign Yankee Clipper mass 28,838 kg service module = SM 108 lunar module = LM 6 callsign Intrepid mass 15,235 kg booster = Saturn V SA… …

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  • 7Nahuel 1A — was a Spacebus 2000NG satellite manufactured by Aérospatiale in Cannes Mandelieu and launched on January 30, 1997 by an Ariane 44L launcher. The satellite was located in the 71.8 degrees slot. It was operated by Nahuelsat S.A., the first… …

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  • 8STS-51-G — Infobox Space mission mission name = STS 51 G insignia = Sts 51 g patch.png shuttle = Discovery launch pad = 39 A launch = June 17, 1985, 11:33:00 UTC landing = June 24, 1985, 13:11:52 UTC Runway 23, Edwards AFB duration = 7d/01:38:52 altitude =… …

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  • 9Thrust-to-weight ratio — is, as its name suggests, the ratio of instantaneous thrust to weight (where weight means weight at the Earth’s surfaceSutton (7th edition pg 442) thrust to weight ratio F/Wg is a dimensionless parameter that is identical to the acceleration of… …

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  • 10Arab Satellite Communications Organization — Infobox Company company name = ARABSAT company company type = foundation = 1976 location = Riyadh, SAU key people = industry = Satellite communication homepage = http://www.arabsat.com//The Arab Satellite Communications Organization (often… …

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