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REAL-GAS EFFECTS ON HYPERSONIC NOZZLE CONTOURS WITH A METHOD OF CALCULATION
The interior ballistics of the fluid controlled solid rocket motor
Some problems in designing a lunar photographic survey mission
A general method for determining optimum thrust nozzle contours for gas-particle flows.
Selection of nozzle contours for a research scramjet engine.
Status of the 260-inch diameter solid rocket motor program.
Using the SPICE System to Help Plan and Interpret Space Science Observations
Level 1 In-Flight Geometric Calibration Algorithm Theoretical Basis
CSPICE - A C Version of JPL's SPICELIB Toolkit