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Application of a lunar landing technique for landing from an elliptic orbit estabilished [NASA TN D-2520] : NASA

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Material type: Text

TextLanguage: English Series: Aeronautics and Space Administration (NASA)Publication details: Washington, D.C. NASA 1964Description: 22pSubject(s):

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NASA technical note

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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	COMPACT STORAGE (BASEMENT)		Not for loan		TR015575 [D-2520]

Total holds: 0

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Previous	Investigation of the dynamic stability and controllability of a towed model of a modified half cone reentry vehicle [NASA TN D-2517]	EEffects of dielectric covers over shunt slots in a waveguide [NASA TN D-2518]	Experimental investigation of slosh suppression effectiveness of annular ring baffles in spherical thanks [NASA TN D-2519]	Application of a lunar landing technique for landing from an elliptic orbit estabilished [NASA TN D-2520]	NASA Technical Note [NASA TN D-3092]: Stress-intensity factors for three-point bend specimens by boundary collocation	NASA Technical Note :INVESTIGATION OF A JET CONDENSER FOR SPACE POWER	NASA Technical Note :EXPERIMENTAL FLUTTER STUDY OF A WING-FUSELAGE CONFIGURATION AT A MACH NUMBER OF 15.4 AND COMPARISON WITH THEORY	Next

NASA technical note

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