Static thrust augmentation of a rocket-ejector system with a heated supersonic primary jet /
"An investigation was conducted in order to evaluate the static thrust augmentation attainable through the use of a rocket-ejector system with a heated supersonic primary jet. This system consisted of a cylindrical mixing tube in conjunction with a supersonic nozzle having an expansion ratio of...
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| Corporate Authors: | , |
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| Format: | Book |
| Language: | English |
| Published: |
Washington, [D.C.] :
National Aeronautics and Space Administration,
1962
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| Series: | NASA technical note ;
D-1261 NASA technical note ; D-1261 |
| Subjects: | |
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