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Title: On-orbit performance of TOPEX/Poseidon electrical power system through its design life of three years

Book ·
OSTI ID:163382
;  [1];  [2]
  1. Orbital Sciences Corp., Germantown, MD (United States)
  2. California Inst. of Technology, Pasadena, CA (United States). Jet Propulsion Lab.

The main objective of the TOPEX Spacecraft is to monitor the World`s oceans for both scientific study of weather and climate prediction, coastal storm warning and maritime safety. TOPEX carries a radar altimeter, a microwave radiometer, a laser retro-reflector array, a frequency unit and an experimental GPS demonstration receiver provided by NASA, and a DORIS doppler tracking receiver and a solid-state radar altimeter provided by CNES, the French Space Agency. The spacecraft with these payloads imposed challenging requirements for the on-board Electrical Power System (EPS). This paper presents an overview of the EPS and its flight performance obtained through telemetry since launch.

OSTI ID:
163382
Report Number(s):
CONF-950729-; TRN: IM9604%%487
Resource Relation:
Conference: 30. intersociety energy conversion engineering conference, Orlando, FL (United States), 30 Jul - 5 Aug 1995; Other Information: PBD: 1995; Related Information: Is Part Of Proceedings of the 30. intersociety energy conversion engineering conference. Volume 1; Goswami, D.Y. [ed.] [Univ. of Florida, Gainesville, FL (United States)]; Kannberg, L.D.; Somasundaram, S. [eds.] [Pacific Northwest Lab., Richland, WA (United States)]; Mancini, T.R. [ed.] [Sandia National Labs., Albuquerque, NM (United States)]; PB: 798 p.
Country of Publication:
United States
Language:
English