BremSat
Class: Technology. Type: RV. Destination: Maximum Payload Orbit. Nation: Germany. Agency: DARA/Bre. Manufacturer: Univeristy of Bremen.

Atomic oxygen, dust particle, microgravity, reentry experiments.

Typical orbit: 158 km circular orbit, 57 deg inclination. Mass: 63 kg (138 lb). Associated Launch Vehicle: Shuttle.


BremSat Chronology
  • 1994 February 3 - BremSat 1 - Launch Site: Cape Canaveral. Launch Vehicle: Shuttle. Mass: 63 kg (138 lb). Perigee: 156 km (96 mi). Apogee: 160 km (90 mi). Inclination: 57.00 deg. Period: 87.70 min.

    Atomic oxygen, dust particle, microgravity, reentry experiments.


Bibliography and Further Reading
  • NASA GSFC Orbital Parameters, .
  • McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
 
 
 
 
 
 
 
 
 

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