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  2. Comparison of orbital launch systems - Wikipedia

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

    [note 2] Liquid-propellant rockets have a motor that feeds liquid propellant(s) into a combustion chamber. Most liquid engines use a bipropellant , consisting of two liquid propellants (fuel and oxidizer) which are stored and handled separately before being mixed and burned inside the combustion chamber.

  3. Comparison of orbital launcher families - Wikipedia

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

    The article is organized into two tables: the first contains a list of currently active and under-development launcher families, while the second contains a list of retired launcher families. The related article " Comparison of orbital launch systems " lists each individual launcher system within any given launcher family, categorized by its ...

  4. Two-stage-to-orbit - Wikipedia

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

    A two-stage-to-orbit (TSTO) or two-stage rocket is a launch vehicle in which two distinct stages provide propulsion consecutively in order to achieve orbital velocity. It is intermediate between a three-stage-to-orbit launcher and a hypothetical single-stage-to-orbit (SSTO) launcher.

  5. Mark 36 SRBOC - Wikipedia

    en.wikipedia.org/wiki/Mark_36_SRBOC

    Two Mark 36 Mod 7 SRBOC launchers aboard the battleship USS Wisconsin during Operation Desert Storm.. The BAE Systems Mark 36 Super Rapid Bloom Offboard Countermeasures Chaff and Decoy Launching System (abbreviated as SRBOC or "Super-arboc") is an American short-range decoy launching system (DLS) that launches radar or infrared decoys from naval vessels to foil incoming anti-ship missiles.

  6. Sylver vertical launching system - Wikipedia

    en.wikipedia.org/wiki/Sylver_Vertical_Launching...

    The launcher comes in several variants, each distinguished by their height. A-35 and A-43 were developed for launching short range surface-to-air missiles, the A-50 for the long-range PAAMS air defense system, and the A-70 launcher for longer missiles such as the MdCN naval land attack cruise missile.

  7. LauncherOne - Wikipedia

    en.wikipedia.org/wiki/LauncherOne

    The rocket had a diameter of 1.6 m (5 ft 3 in) for the first stage and 1.3 m (4 ft 3 in) for the second stage and payload fairing. [ 4 ] On the 24th of October 2019, the company announced plans to develop a three-stage variant that would be capable of launching 100 kg (220 lb) to the Moon , 70 kg (150 lb) to Venus , or 50 kg (110 lb) to Mars .

  8. Air-launch-to-orbit - Wikipedia

    en.wikipedia.org/wiki/Air-launch-to-orbit

    Orbital's Stargazer launches Pegasus carrying the three Space Technology 5 satellites in the skies of California, 2006. Air-launch-to-orbit (ALTO) is the method of launching smaller rockets at altitude from a heavier conventional horizontal-takeoff aircraft, to carry satellites to low Earth orbit.

  9. S-350 missile system - Wikipedia

    en.wikipedia.org/wiki/S-350_missile_system

    9M100 guided missiles; 10–15 km (6.2–9.3 mi) range; infrared passive homing; aerodynamic control surfaces and thrust vectoring; maximum maneuver 60 G-20 surfaces. 9M100 can be quad packed in the naval version. [10] Basic performance characteristics of the S-350: [11] [12] Maximum number of simultaneously engaged targets: Aerodynamic – 16