This report describes test procedures for determining the possibility of vernier motor exhaust impingement heating. A one-tenth scale model rocket and an altitude chamber were utilized.
Scale Atlas Vernier Rocket Flame Expansion Studies
1960
28 pages
Report
No indication
English
Combustion & Ignition , Rocket Engines & Motors , Missile Technology , Surface to surface missiles , Rocket nozzles , Flame propagation , Vernier rocket engines , High altitude , Simulation , Guided missile models , Exhaust flames , Stabilization , Shock waves , Thermal radiation , Compressible flow , Atlas , Impingement heating , Xsm-65 missiles
Continuously-Variable Vernier Scale
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