Design of calorimeters to obtain flight data at lunar reentry velocity and equations to convert telemetered temperature responses into heat flux valves
CONSIDERATIONS IN DESIGN OF CALORIMETERS FOR THE PROJECT FIRE SUPERORBITAL RE-ENTRY TEST VEHICLE
1945-01-01
Preprint
No indication
English
Considerations in design of calorimeters for project FIRE superorbital re-entry test vehicle
Engineering Index Backfile | 1963
|Considerations in Design of Calorimeters for the Project FIRE Superorbital Re-Entry Test Vehicle
SAE Technical Papers | 1963
|Non-lifting entry-vehicle design for superorbital velocities
Engineering Index Backfile | 1963
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