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  2. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio

  3. Atlas V - Wikipedia

    en.wikipedia.org/wiki/Atlas_V

    The Centaur upper stage uses a pressure-stabilized propellant-tank design and cryogenic propellants. The Centaur stage for Atlas V is stretched 1.7 m (5 ft 7 in) relative to the Atlas IIAS Centaur and is powered by either one or two Aerojet Rocketdyne RL10A-4-2 engines, each engine developing a thrust of 99.2 kN (22,300 lb f).

  4. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Falcon 9 Block 5, the most prolific ... Atlas V 551 United States: ULA: 58.3 m ... Falcon Heavy United States ...

  5. Atlas (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Atlas_(rocket_family)

    It was pressure in the tanks that gave the rigidity required for space flight. In order to save weight they were not painted and needed a specially designed oil to prevent rust. This was the original use of WD-40 water displacement oil. [5] The SM-65 Atlas was used as a first stage for satellite launch vehicles for half a century.

  6. Centaur (rocket stage) - Wikipedia

    en.wikipedia.org/wiki/Centaur_(rocket_stage)

    The Atlas V can fly in multiple configurations, but only one affects the way Centaur integrates with the booster and fairing: the 5.4 m (18 ft) diameter Atlas V payload fairing attaches to the booster and encapsulates the upper stage and payload, routing fairing-induced aerodynamic loads into the booster. If the 4 m (13 ft) diameter payload ...

  7. SpaceX launch vehicles - Wikipedia

    en.wikipedia.org/wiki/SpaceX_launch_vehicles

    Falcon Heavy (FH) is a super heavy lift space launch vehicle designed and manufactured by SpaceX. The Falcon Heavy is a variant of the Falcon 9 launch vehicle comprising three Falcon 9 first stages: a reinforced center core, and two additional side boosters. All three boosters are capable of being recovered and reused, although most flights use ...

  8. Two-stage-to-orbit - Wikipedia

    en.wikipedia.org/wiki/Two-stage-to-orbit

    As of 2023, SpaceX and NASA are the only launch providers which have achieved first-stage reuse of an orbital vehicle with SpaceX’s two-stage Falcon 9 and 2.5-stage Falcon Heavy, and NASA’s Space Shuttle Solid Rocket Boosters. Rocket Lab has recovered multiple first stages of their Electron rocket, but has not flown it again.

  9. Falcon 9 Block 5 - Wikipedia

    en.wikipedia.org/wiki/Falcon_9_Block_5

    Falcon 9 Block 5 is a partially reusable, human-rated, two-stage-to-orbit, medium-lift launch vehicle [c] designed and manufactured in the United States by SpaceX. It is the fifth major version of the Falcon 9 family and the third version of the Falcon 9 Full Thrust .