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Reusable Launch Vehicle: Technology Development and Test Program
recommends that a clear path toward certifying readiness for launch of flight-critical hardware be developed.
Weight requirements (not only the 4 lb/ft2 given in the decision criteria) must be defined for each vehicle concept.
NOTES
1. Aldrich, Arnold D. 1993. Access to Space Study: Report to the Administrator. Washington, D.C.: National Aeronautics and Space Administration.
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