Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5/
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| Corporate Authors: | , , |
| Other Authors: | |
| Format: | Book |
| Language: | English |
| Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1984
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| Series: | NASA technical paper
2283 |
| Subjects: |