Object: To determine the stagnation point heating rate to spherical and cylindrical bodies of the same diameter at various locations in the highly expanded exhaust jet of a scale vernier rocket.
Further Investigation of Heating Rates to Spherical and Cylindrical Bodies in a 1/10 Scale Atlas Vernier Rocket Engine Exhaust
1959
17 pages
Report
No indication
English
Rocket Engines & Motors , Physics , Aircraft , Vernier rocket engines , Exhaust flames , Airframes , Heat transfer , Calorimeters , Surface to surface missiles , Model tests , Scale , Spheres , Cylindrical bodies , Stainless steel , Test equipment , Temperature , Stabilization , Liquid propellant rocket engines , Captive tests , Atlas , Graphs(Charts) , Steel 1050 , Xsm-65 missiles
Scale Atlas Vernier Rocket Flame Expansion Studies
NTIS | 1960
|Study of Rocket Engine Exhaust Products
NTIS | 1964
|