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ANALYSIS OF COMBINATIONS OF ALTITUDE AND DESCENT RATE FOR SAFE ABORT DURING TERMINAL PHASE OF LUNAR LANDING

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BookPublisher: Nasa, Washington, D.C. 1966Description: 27.DDC classification: NASA | TN D-3525

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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 TN D-3525 (Browse shelf)	Not for loan		TR12562

Total holds: 0

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Previous	NASA TN D-3522 EXPERIMENTS TO DETERMINE THE STRENGTH OF FILAMENT-WOUND CYLINDERS LOADED IN AXIAL COMPRESSION	NASA TN D-3523 HYPERSONIC LAMINAR VISCOUS INTERACTION EFFECTS ON THE AERODYNAMICS OF TWO-DIMENSIONAL WEDGE AND TRIANGULAR PLANFORM WINGS	NASA TN D-3524 VISUAL SIMULATION OF LUNAR ORBIT EXTABLISHMENT USING A SIMPLIFIED GUIDANCE TECHNIQUE	NASA TN D-3525 ANALYSIS OF COMBINATIONS OF ALTITUDE AND DESCENT RATE FOR SAFE ABORT DURING TERMINAL PHASE OF LUNAR LANDING	NASA TN D-3526 STAGNATION AND STATIC PRESSURES ON A NOSE-MOUNTED 15 (DEGRE) CONICAL PROBE WITH VARIOUS FOREBODY CONFIGURATIONS	NASA TN D-3527 METALLOGRAPHIC STUDY OF DISPERSION-STRENGTHENED ALLOYS AFTER FAILURE IN STRESS RUPTURE	NASA TN D-3528 GOLD REDUCTION AS A MEANS OF REDUCING EMBRITTLEMENT OF A COBALT-BASE ALLOY (L-605)	Next

Bound With Nasa Tn D-3521-3524,3526-3530

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