Launch vehiclesSee also what's at your library, or elsewhere.
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Filed under: Launch vehicles Round trip to orbit : human spaceflight alternatives : special report. (Congress of the United States, Office of Technology Assessment :, 1989), by United States Congress Office of Technology Assessment (page images at HathiTrust) 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) Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications (National Aeronautics and Space Administration ;, 1966), by Roger H. Fournier and Langley Research Center (page images at HathiTrust) Technology requirements for future Earth-to-geosynchronous orbit transportation systems. Volume 1, Executive summary (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Vincent A. Calouri, James C. Jenkins, Robert T. Conrad, Langley Research Center, and Boeing Aerospace Company (page images at HathiTrust) Kinematic analysis of the engine and pump inlet duct gimbal joint system in the s-1c stage of the saturn v vehicle (National Aeronautics and Space Administration, 1964), by F. F. Garcia and George C. Marshall Space Flight Center (page images at HathiTrust)
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