High performance arrays for lightweight spacecraftJPL is developing the solar arrays for NASA's ultralightweight spacecraft, the Lunar Get-Away Special (L-GAS), which requires 1 kWe after its slow passage through the Van Allen Belts. The solar array design developed for the mission extended recent NASA-developed photovoltain array technology to power levels well below those conventionally considered practical for deployable lightweight array technology. It has become feasible by these means to consider the design of lightweight spacecraft which require up to 3 kWe at the begining of their service life.
Document ID
19900031773
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stella, Paul M. (JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: AIAA/DARPA Meeting on Lightweight Satellite Systems