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Title: The Astro Edge solar array for the NASA SSTI Clark Spacecraft

Conference ·
OSTI ID:177670

The Astro Edge solar array is a new and innovative reflective low concentrator power generating system which has been selected for the CTA Incorporate/Lockheed Martin Clark spacecraft under the NASA Small Spacecraft Technology Initiative (SSTI) program. In support of this program, Astro Aerospace Corporation has produced one qualification and two flight solar array wings to support a July 1996 launch. The Astro Edge solar array was selected as a new technology to benefit future NASA, military and commercial missions by providing high specific power, high deployed stiffness, low stowed volume, low risk, and cost reduction features which meet the agency`s `better, faster, cheaper` goals. This novel array accounts for five of the thirty-six advanced technologies which the Clark spacecraft will demonstrate. A brief SSTI Astro Edge solar array program overview is presented. Completed qualification and acceptance testing is discussed. Finally, the major discriminators which make the Astro Edge solar array `better, faster, cheaper` technology are provided.

Research Organization:
NASA Lewis Research Center, Cleveland, OH (United States)
OSTI ID:
177670
Report Number(s):
N-96-15042; NASA-CP-10180; NAS-1.55:10180; E-9943; NIPS-95-05337; CONF-9510288-; TRN: 9615069
Resource Relation:
Conference: 14. space photovoltaic research and technology conference, Cleveland, OH (United States), 24-26 Oct 1995; Other Information: PBD: Oct 1995; Related Information: Is Part Of Proceedings of the 14th Space Photovoltaic Research and Technology Conference (SPRAT 14); Landis, G.; PB: 47 p.
Country of Publication:
United States
Language:
English