Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements /
Leslie L. Scalzott and Fred Teren.

APA Citation

Scalzott, L. L., Teren, F., United States. National Aeronautics and Space Administration. (1968). Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements. Washington, D.C.: National Aeronautics and Space Administration .

MLA Citation

Scalzott, Leslie L, Fred Teren, and United States. National Aeronautics and Space Administration. Load Relief Autopilot Analysis to Minimize Launch Vehicle Peak Thrust Vector Deflection Requirements. Washington, D.C.: National Aeronautics and Space Administration , 1968.