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EFFECT OF LIFT ON SEPARATION DISTANCE AND LOADS FOR AN ABORTING VEHICLE AT MAXIMUM DYNAMIC PRESSURE OF A LUNAR MISSION

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BookPublisher: Nasa, Washington, D.C. 1963Description: 25.DDC classification: NASA | TN D-1775

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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-1775 (Browse shelf)	Not for loan		TR13159

Total holds: 0

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Previous	NASA TN D-1772 STUDY OF INERTIAL NAVIGATION ERRORS DURING REENTRY TO THE EARTH`S ATMOSPHERE	NASA TN D-1773 SIMULATOR STUDY OF THE LATERAL-DIRECTIONAL HANDLING QUALITIES OF A LARGE FOUR-PROPALLERED STOL TRANSPORT AIRPLANE	NASA TN D-1774 AERODYNAMIC CHARACTERISTICS OF A FULL-SCALL PROPALLER TESTED WITH BOTH RIGID AND FLAPING BLADES AND WITH CYCLIC PITCH CONTROL	NASA TN D-1775 EFFECT OF LIFT ON SEPARATION DISTANCE AND LOADS FOR AN ABORTING VEHICLE AT MAXIMUM DYNAMIC PRESSURE OF A LUNAR MISSION	NASA TN D-1776 AERODYNAMIC CHARACTERISTICS OF A FLEXIBLE-CANOPY PARAGLIDER MODEL AT A MACH NUMBER OF 4.5 FOR ANGLES OF ATTACK TO 360 DEGREE AND SIDESLIP ANGLES FROM 0 DEGREE TO 90 DEGREE	NASA TN D-1777 AIRCRAFT VORTEX WAKES IN RELATION TO TERMINAL OPERATIONS	NASA TN D-1778 ESTIMATES OF ATTENUATION AND REFLECTION OF TELEMETERING SIGNALS BY IONIZED FLOW FIELDS SURROUNDING TYPICAL REENTRY BODIES	Next

Bound With Nasa Tn D-1771-74,1776-80

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