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THE CRITICAL INCLINATION PROBLEM IN SATELLITE ORBIT THEORY

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Material type: Text

TextPublication details: Nasa, Washington, D.C. 1962Description: 66DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TR R-148 (Browse shelf(Opens below))	Not for loan		TR12457

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	NASA TR R-145 AN INVESTIGATION OF THE VIBRATION CHARACTERISTICS OF PRESSURIZED THIN-WALLED CIRCULAR CYLINDERS PARTLY FILLED WITH LIQUID	NASA TR R-146 LAMINARBOUNDARY-LAYER SEPARATION INDUCED BY FLARES ON CYLINDERS AT ZERO ANGLE OF ATTACK	NASA TR R-147 COMPUTATION OF SATELLITE ORBITS BY THE HANSEN METHOD AS MODIFIED BY MUSEN	NASA TR R-148 THE CRITICAL INCLINATION PROBLEM IN SATELLITE ORBIT THEORY	NASA TR R-149 AERODYNAMIC ANALYSIS OF TEKTITES AND THEIR PARENT BODIES	NASA TR R-150 THEORETICAL STUDY OF CAMBER FLUTTER CHARACTERISTICS OF MONCOQUE AND MULTIWEB WINGS	NASA TR R-153 - EXPERIMENTAL STUDY OF THE PRESSURE AND HEAT-TRANSFER DISTRIBUTION ON A 70(DEGREE) SWEEP SLAB DELTA WING IN HYPERSONIC FLOW	Next

Bound With Nasa Tr R-141-147,149-50

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