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LINEAR THEORY OF IMPULSIVE VELOCITY CORRECTIONS FOR SPACE MISSION GUIDANCE

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Material type: Text

TextLanguage: English Series: NASA Technical NotePublication details: NASA, Washington, D.C. 1966Description: 43Subject(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-3365	Not for loan		TR14075

Total holds: 0

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Previous	PROPELLANT VAPORIZATION AS A CRITERION FOR ROCKET-ENGINE DESIGN; EXPERIMENTAL PERFORMANCE, VAPORIZATION, AND HEAT-TRANSFER RATES WITH VARIOUS PROPELLANT COMBINATIONS [NASA MEMO 12-29-58E]	APOLLO INFRARED ACQUISITION AND TRACKING SYSTEM	FLIGHT MEASUREMENTS OF BOUNDARY-LAYER NOISE ON THE X-15	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	Next

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

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