theoretical performance of rocket engines using gaseous hydrogen in the ideal state at stagnation temperatures up to 200,000 R
Title:
theoretical performance of rocket engines using gaseous hydrogen in the ideal state at stagnation temperatures up to 200,000 R
Author:
Roback, Richard.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, 1967.
Physical Description:
vi, 215 pages : illustrations ; 27 cm.
Language:
English
Format :
Book