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Static thrust augmentation of a rocket-ejector system with a heated supersonic primary jet

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BookPublisher: Washington NASA 1962Description: 27p.

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-1261 (Browse shelf)	Not for Issue		65526

Total holds: 0

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Previous	NASA TN D 41-50 GROUND MEASUREMENTS OF THE SHOCK-WAVE NOISE FROM AIRPLANES IN LEVEL FLIGHT AT MACH NUMBERS TO 1.4 AND AT ALTITUDES TO 45,000 FEET [NASA TN D-48]	NASA TN D-1 A STUDY OF THE ACOUSTIC FATIGUE CHARACTERISTICS OF SOME FLAT AND CURVED ALUMINIUM PANELS EXPOSED TO RANDOM AND DISCRETE NOISE	NASA TN D-1211 An investigation of the effects of the time lag due to long transmission distances upon remote control.[TN D-1211 -- TN D-1220]	NASA TN D-1261 Static thrust augmentation of a rocket-ejector system with a heated supersonic primary jet	NASA TN D-1301 Aerodynamic characteristics of a 4-foot-diameter ducted fan mounted on the tip of a semispan [NASA TN D-1301]	NASA TN D-1311 Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms	NASA TN D-1394 A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at mach numbers of 1.61 and 2.01 for a reflex cambered wind and a cambered and twisted wind having the same swept planform. [NASA TN D-1393]	Next

NASA TN-1261

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