Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

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:
National Aeronautics and Space Administration, Cleveland, OH (United States). Lewis Research Center
OSTI ID:
177670
Report Number(s):
N--96-15042; NASA-CP--10180; NAS--1.55:10180; E--9943; NIPS--95-05337; CONF-9510288--
Country of Publication:
United States
Language:
English

Similar Records

Development of the Astro Edge solar array
Conference · Fri Dec 30 23:00:00 EST 1994 · OSTI ID:191177

An introduction to the Astro Edge solar array
Conference · Thu Sep 01 00:00:00 EDT 1994 · OSTI ID:36441

EOS AM-1 GaAs/Ge flexible blanket solar array verification test program results
Conference · Tue Dec 30 23:00:00 EST 1997 · OSTI ID:347781