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  2. VTVL - Wikipedia

    en.wikipedia.org/wiki/VTVL

    The Soviet Union did some development work on a vertically landing crewed capsule called Zarya in the late 1980s. [7] The McDonnell Douglas DC-X was a 1/3 scale uncrewed prototype SSTO VTVL launch vehicle that flew several test flights in the 1990s. Its first successful flight was in 1993.

  3. Scaled Composites Stratolaunch - Wikipedia

    en.wikipedia.org/wiki/Scaled_Composites_Stratolaunch

    Stratolaunch has a twin-fuselage configuration, each 238 ft (73 m) long and supported by 12 main landing gear wheels and two nose gear wheels, for a total of 28 wheels. [17] The twin-fuselage configuration is similar to the Scaled Composites White Knight Two. [14] Each fuselage has its own empennage. [38]

  4. Landing gear - Wikipedia

    en.wikipedia.org/wiki/Landing_gear

    The landing gear represents 2.5 to 5% of the maximum takeoff weight (MTOW) and 1.5 to 1.75% of the aircraft cost, but 20% of the airframe direct maintenance cost. A suitably-designed wheel can support 30 t (66,000 lb), tolerate a ground speed of 300 km/h and roll a distance of 500,000 km (310,000 mi) ; it has a 20,000 hours time between overhaul and a 60,000 hours or 20 year life time.

  5. Dream Chaser - Wikipedia

    en.wikipedia.org/wiki/Dream_Chaser

    The main landing gear was tested in a similar way in February 2012. The nose gear landing test was the last milestone to be completed before the free flight approach and landing tests scheduled for later in 2012. [45] In August 2012, SNC completed CCiCap Milestone 1, or the 'Program Implementation Plan Review'.

  6. Scaled Composites - Wikipedia

    en.wikipedia.org/wiki/Scaled_Composites

    Scaled Composites was established in 1982 and purchased by the Beech Aircraft Corporation in 1985, as a result of the collaboration on the Starship project. In 1988, Beech's parent company, Raytheon, sold Scaled back to Rutan, who then sold it to Wyman-Gordon.

  7. RLV Technology Demonstration Programme - Wikipedia

    en.wikipedia.org/wiki/RLV_Technology...

    The full-scale RLV is expected to use retractable landing gear. [ 10 ] By May 2015, engineers at the Vikram Sarabhai Space Centre (VSSC) in Thumba Equatorial Rocket Launching Station were installing thermal tiles on the outer surface of the RLV-TD to protect it against the intense heat during atmospheric reentry . [ 11 ]

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  9. Space Shuttle orbiter - Wikipedia

    en.wikipedia.org/wiki/Space_Shuttle_orbiter

    The hydraulic pressure generated was also used to control all of the orbiter's flight control surfaces (the elevons, rudder, speed brake, etc.), to deploy the landing gear of the orbiter, and to retract the umbilical hose connection doors located near the rear landing gear, which supplied the orbiter's SSMEs with liquid hydrogen and oxygen from ...

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