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Menasco built the landing gear that allowed the space shuttle to land on a runway. [8] It manufactured the landing gear of the Orbiter structure launched in 1977 from a 300-M steel coated in titanium-cadmium plating. [9]
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 ...
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]
The orbiter was 56 kilometers (184,000 ft) high and travelling at Mach 15.6. Space Shuttle Discovery as it approaches the International Space Station during the STS-114 on 28 July 2005. The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the extreme 1,650 °C (3,000 °F ) heat of ...
Space Shuttle Enterprise (Orbiter Vehicle Designation: OV-101) was the first orbiter of the Space Shuttle system. Rolled out on September 17, 1976, it was built for NASA as part of the Space Shuttle program to perform atmospheric test flights after being launched from a modified Boeing 747. [1]
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.
Orbiter Tow Vehicle. This unit is very much like the typical towing units used for large aircraft. However, it was equipped with a special towing bar designed specifically for the orbiter. It was used to move the orbiter from the landing facility to the OPF. It also is used for moving the orbiter from the OPF to the VAB. Mobile Ground Power Unit.
The orbiter, its science payload and ground control infrastructure are technology demonstrators. The orbiter will also be tasked with surveying lunar resources such as water ice, uranium, helium-3, silicon, and aluminium, and produce a topographic map to help select future lunar landing sites. Hakuto-R Mission 1: Japan 21 March 2023
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