- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Tests were conducted in the NASA/LaRC 8 foot transonic wind tunnel from March 26 through 31, 1976. The model was a 0.015 scale SSV Orbiter with forebody modifications to simulate slight reductions in the reusable surface insulation (RSI) thickness. Six component aerodynamic force and moment data were obtained at Mach numbers from 0.35 to 1.20 over an angle of attack range from -2 deg to 20 deg at sideslip angles of 0 deg and 5 deg.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19770005165.
Accession ID: 77N12108.
- No Copyright.
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