Centaur launch vehicleSee also what's at your library, or elsewhere.
|
Filed under: Centaur launch vehicle- Payload capabilities of Saturn IB-Centaur for launch opportunities to Mars in 1971, 1973, and 1975 and to Venus in 1972 and 1973 (National Aeronautics and Space Administration ;, 1966), by Gary D. Sagerman, Tim J. Kreiter, and Lewis Research Center (page images at HathiTrust)
- Interstage adapter panel flutter on Atlas-Centaur AC-2, AC-3, and AC-4 vehicles (National Aeronautics and Space Administration ;, 1965), by Tilak R. Lall and Lewis Research Center (page images at HathiTrust)
- Comparison of direct and indirect ascent modes for the 1969 Mars opportunity with an Atlas-Centaur launch vehicle (National Aeronautics and Space Administration ;, 1965), by Tim J. Kreiter and Lewis Research Center (page images at HathiTrust)
- Static and dynamic characteristics of Centaur gimbal system under thrust load (National Aeronautics and Space Administration ;, 1966), by Robert J. Antl, Larry D. Plews, David W. Vincent, and Lewis Research Center (page images at HathiTrust)
- Balloon tank skin strain measurements at liquid-hydrogen temperature on Centaur flight vehicle (National Aeronautics and Space Administration ;, 1965), by Tilak R. Lall, William F. Lang, Frank A. Maruna, and Lewis Research Center (page images at HathiTrust)
- Comparison of propellant sloshing parameters obtained from model and full-size Centaur liquid-oxygen tanks (National Aeronautics and Space Administration ;, 1966), by Andrew J. Stofan and Lewis Research Center (page images at HathiTrust)
- Atlas-Centaur-Surveyor longitudinal dynamics test (National Aeronautics and Space Administration ;, 1967), by Theodore F. Gerus, George L. Kusic, John A. Housely, and Lewis Research Center (page images at HathiTrust)
Items below (if any) are from related and broader terms. |