The Online Books Page

Multistage rocket vehicles

See also what's at your library, or elsewhere.

• Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 (National Aeronautics and Space Administration, 1959), by Ross B. Robinson and Langley Research Center (page images at HathiTrust)
• Payload vibration data measured during five flights of a two-stage solid-propellant launch vehicle (National Aeronautics and Space Administration, 1962), by Sherman A. Clevenson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Supersonic aerodynamic characteristics of a 1/6-scale model of the final two stages of the Argo D-4 four-stage rocket vehicle (National Aeronautics and Space Administration ;, 1965), by Clyde Hayes, William A. Corlett, and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.