Flight data from Saturn I have established base thermal environment of eight-engine LOX/RP-1 rockets; plume radiation levels, total heating rates, and base gas temperatures have been measured on first stage of Block I and II vehicles; some heating data also were obtained for six-engine LOX/LH2, S-IV second-stage base; flight instrumentation, data reduction techniques, and evaluation problems are discussed along with correlation of flight results to long- and short-duration model tests.
Summary of Saturn I base thermal environment
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 3 , n 4
1966
9 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Summary of saturn i base thermal environment.
NTRS | 1965
|Summary of Saturn I base thermal environment.
AIAA | 1966
|Summary of saturn i base thermal environment
AIAA | 1965
|Summary of Saturn I base thermal environment.
NTRS | 1966
|