Description of vehicle system and flight tests of nine Trailblazer I reentry physics research vehicles
William N. Gardner, Clarence A. Brown, Langley Research Center, Allen B. Henning, W. Ray Hook, Reginald R. Lundstrom, Ira W. Ramsey, United States. National Aeronautics and Space Administration
National Aeronautics and Space Administration, 1964 - Technology & Engineering - 89 pages
What people are saying - Write a review
We haven't found any reviews in the usual places.
aerodynamic altitude angle of attack apogee booster camera location canted Coquina Beach cycles per second data were obtained diaphragm dispersion experimental reentry physics feet Figure 23 fin misalinements first-stage flight tests flight-path angle fourth-stage ignition heating rate horizontal range ICBM speeds incoming stages Langley Research Center Launch angle Lincoln Laboratory Lundstrom NASA TN NINE TRAILBLAZER nominal performing experimental reentry phenolic photograph radio beacon transmitter reentry body reentry physics research reentry trajectory reentry weight right ascension S-band Second-stage shown in figure six-stage solid-fuel rocket sixth stage sixth-stage ignition sixth-stage reentry spherical rocket motor spin rate produced spin stability stagnation point star background TESTS OF NINE Thin aluminum third-stage burning third-stage burnout third-stage fins third-stage motor third-stage telemeter titanium trace unchopped TRAILBLAZER I REENTRY Trailblazer I vehicles Trailblazer Ie trajectory for Trailblazer transverse accelerations unique six-stage solid-fuel vehicle spin rate velocity package wall temperature Wallops Island William N