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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. List of Android launchers - Wikipedia

    en.wikipedia.org/wiki/List_of_Android_launchers

    The topic of this article may not meet Wikipedia's notability guideline for stand-alone lists. Please help to demonstrate the notability of the topic by citing reliable secondary sources that are independent of the topic and provide significant coverage of it beyond a mere trivial mention.

  5. 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 .

  6. Sylver vertical launching system - Wikipedia

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

    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. The numbers refer to the approximate length of the missile which can be accommodated, in decimetres, i.e. the A-43 can ...

  7. 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.

  8. AT4 - Wikipedia

    en.wikipedia.org/wiki/AT4

    In US military use, the launcher can be fitted with the AN/PAQ-4C, AN/PEQ-2, or the AN/PAS-13 night sights. The AT4 requires little training and is quite simple to use, making it suitable for general issue.

  9. Multi-Mission Launcher - Wikipedia

    en.wikipedia.org/wiki/Multi-Mission_Launcher

    IFPC Inc 2-I launch of an AIM-9X Sidewinder Missile IFPC Longbow vs MQM-170 Outlaw 25 March 2016 Tamir Firing from IFPC Inc 2-I Multi Mission Launcher. The Multi-Mission Launcher (MML) is an open-systems architecture multi-role missile launching system created by the United States Army's Aviation and Missile Research, Development, and Engineering Center.