DRAGONSat

DRAGONSat
DRAGONSat as photographed after its release from Space Shuttle Endeavour's payload bay
COSPAR ID2009-038B Edit this at Wikidata
SATCAT no.35690Edit this on Wikidata
Start of mission
Launch dateJuly 30, 2009 (UTC) (2009-07-30Z)
RocketSpace Shuttle Endeavour
Launch siteKennedy LC-39A
End of mission
DisposalFailed to separate from companion
Orbital parameters
Reference systemgeocentric
RegimeLEO
Inclination51.7°

DRAGONSat (Dual RF Astrodynamic GPS Orbital Navigator Satellite) was a 2000s pair of nanosatellites that were to demonstrate autonomous rendezvous and docking (ARD) in low Earth orbit (LEO) for NASA. It was intended to gather flight data with a global positioning system (GPS) receiver strictly designed for space applications to gather flight data in the space environment. ARD is the capability of two independent spacecraft to rendezvous in orbit and dock without crew intervention. The mission failed when the DRAGONSats failed to separate from their carrier spacecraft.

One DRAGONSat was built by the University of Texas and the other one was built by Texas A and M University, the Space Shuttle Payload Launcher (SSPL), These satellite projects were planned to rendezvous and dock with each other in space without the benefit of human intervention.

DRAGONSat was planned to be an eight-year program with a launch of the satellites approximately every two years. The first three missions were to test individual components and subsystems while the final mission was to culminate with the successful docking of two satellites. Each mission was planned to build on the previous mission culminating in a fully autonomous rendezvous and docking mission. Both universities were required to use GPS receivers designed by NASA in order to determine its functionality. One of the objectives was to demonstrate precision real-time navigation capability as well as precision relative navigation between the two satellites. [1]