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ANALYSIS OF FLOW-SYSTEM STARTING DYNAMICS OF TURBOPUMP-FED LIQUID-PROPELLANT ROCKET

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BookPublisher: Nasa, Washington, D.C. 1959Description: 45.DDC classification: NASA | MEMO 4-21-59E -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA MEMO 4-21-59E - (Browse shelf)	Not for loan		TR7710

Total holds: 0

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Previous	NASA MEMO 4-17-59L - AIRPLANE MEASUREMENTS OF ATMOSPHERIC TURBULENCE AT ALTITUDES BETWEEN 20,000 AND 55,000 FEET FOR FOUR GEOGRAPHIC AREAS	NASA MEMO 4-19-59L - Flight performance of a transonic turbine-driven propeller designed for minimum noise	NASA MEMO 4-20-59L TRANSONIC AERODYNAMIC CHARACTURISTICS OF A 45DEGREE SWEPT-WING-FUSELAGE MODEL WITH A FINNED AND UNFINNED BODY PYLON-MOUNTED BENEATH THE FUSELAGE OR WING, INCLUDING MEASUREMENTS OF BODY LOADS	NASA MEMO 4-21-59E - ANALYSIS OF FLOW-SYSTEM STARTING DYNAMICS OF TURBOPUMP-FED LIQUID-PROPELLANT ROCKET	NASA MEMO 4-21-59L INVESIGATION OF THE CHAACTERISTICS OF AN ACCELERATION-TYPE TAKE-OFF INDICATOR IN A LARGE JET AIRPLANE	NASA MEMO 4-22-59E - PRELIMINARY ANALYSIS OF THE EFFECT OF FLOW SEPARATION DUE TO ROCKET JET PLUMING ON AIRCRAFT DYNAMIC STABILITY DURING ATMOSPHERIC EXIT	NASA MEMO 4-22-59L LOW-SPEED LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION INCLUDING EFFECTS OF CANARD AND WING TRAILING-EDGE FLAP CONTROLS IN COMBINATION	Next

Bound With Nasa Memo 4-6-59e-4-30-59e

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