SpaceDev, USA.
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Associated Countries
Associated Spacecraft
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Rocket Chair American manned lunar lander. Study 2005. In 2005 SpaceDev resurrected the 1960 NASA Langley individual crew lunar lander concept. More...
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Dream Chaser American manned spaceplane. Study 2016. A six-passenger human space transport system announced in 2006 by SpaceDev, based on the ten-passenger HL-20 Personnel Launch System developed by NASA Langley in the 1980's. More...
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NEAP American asteroid probe. Study 2002. Near Earth Asteroid Prospector (NEAP) was SpaceDev's first conceived commercial deep-space mission. The mission was planned as the first deep-space mission defined and executed by a non-governmental entity. More...
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MoTV American space tug. Study 2003. SpaceDev design for a low-cost, restartable hybrid propulsion space tug or upper stage. More...
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SpaceDev ILO American radio astronomy satellite. Study 2003. Unmanned lunar radio astronomy observatory concept, designed to be landed on the South Pole. More...
Associated Engines
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MTV Motor SpaceDev N2O/Solid hybrid rocket engine. Upper stages. Small hybrid rocket motor designed for use in the Maneuver and Transfer Vehicle, an upper stage orbital transfer motor. Tested 2001. More...
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SBIR Hybrid SpaceDev N2O/Solid hybrid rocket engine. 1100 kN. First stage. Upper-stage hybrid propulsion system, part of 2004 Phase 2 of SBIR contract from AFRL for a hybrid rocket motor-based small launch vehicle project. More...
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SpaceDev Hybrid SpaceDev N2O/Solid hybrid rocket engine. 73.5 kN. Rocketplane boost. Out of production. Isp=250s. Used on Tier One launch vehicle. First flight 2002. More...
See also
SpaceDev Chronology
2003 January 13 - .
00:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Delta.
Launch Vehicle:
Delta 7320-10.
LV Configuration: Delta 7320-10.
- CHIPSat - .
Payload: CHIPSat BD 2. Mass: 85 kg (187 lb). Nation: USA. Agency: NASA. Manufacturer: SpaceDev. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: CHIPSat. USAF Sat Cat: 27643 . COSPAR: 2003-002B. Apogee: 601 km (373 mi). Perigee: 585 km (363 mi). Inclination: 94.0070 deg. Period: 96.39 min. Summary: Astrophysics mission. Delayed from March 30, May 12, August 30, September 10, December 15 and 20, 2002; and Jan. 11 and 12, 2003..
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