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Class: Technology. Type: RV. Destination: Maximum Payload Orbit. Nation: Germany. Agency: DARA/Bre. Manufacturer: University of Bremen. Atomic oxygen, dust particle, microgravity, reentry experiments. Typical orbit: 158 km circular orbit, 57 deg inclination. Mass: 63 kg (138 lb).
BremSat Chronology - 1994 February 3 - BremSat 1 - Launch Site: Cape Canaveral. Launch Complex: LC39A. 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:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- NASA GSFC Orbital Parameters,
- McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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