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COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN -OXYGEN ROCKET ENGINE

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Material type: Text

TextLanguage: English Series: NASA Technical NotePublication details: Nasa, Washington, D.C. 1966Description: 32Subject(s):

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Holdings
Item type	Current library	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-3368	Not for loan		TR14078

Total holds: 0

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Previous	LINEAR THEORY OF IMPULSIVE VELOCITY CORRECTIONS FOR SPACE MISSION GUIDANCE	ANGLE-OF ATTACK ANALYSIS FOR PROJECT FIRE 1 PAYLOAD REENTRY FLIGHT	THEORETICAL METHOD FOR DERVIVING AN EARTH-CENTERED DATUM FROM OPTICAL OBSERVATIONS OF THE EARTH'S HORIZON FROM AN EARTH SATELLITE	COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN -OXYGEN ROCKET ENGINE	PENETRATION OF POLYETHYLENE INTO SEMI-INFINITE 2024-T351 ALUMINUM UP TO VELOCITIES OF 37,000 FEET PER SECOND	A PARAMETRIC STUDY OF FACTORS INFLUENCING THE DEEP-STALL PITCH-UP CHARACTERISTICS OF T-TAIL TRANSPORT AIRCRAFT	FATIGUE LIFE OF 120-MM BORE BALL BEARINGS AT 600 DEGREE F WITH FLUORCARBON,POLYPHENYL ETHER, AND SYNTHETIC PARAFFINIC BASE LUBRICANTS.[NASA TN D-4850]	Next

Technical Reports D-3361-70
Bound Vol. No.64318; contents: TR14072-80

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