NASA NTRS · 19930006443
System specification for the reusable reentry satellite
Abstract
The RRS design shall provide a relatively inexpensive method of access to micro and fractional gravity space environments for an extended period of time, with eventual intact recovery on the surface of the Earth. This specification establishes the performance, design, development, and test requirements for the Reusable Reentry Satellite (RRS) system.
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1991-02-01. System specification for the reusable reentry satellite. https://ntrs.nasa.gov/citations/19930006443
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