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OPERATIONAL FEATURES OF THE LANGLEY LUNAR LANDING RESEARCH FACILITY

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BookPublisher: Nasa, Washington, D.C. Description: 36.DDC classification: NASA | TN D-3828

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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-3828 (Browse shelf)	Not for loan Untraceable		TR12520

Total holds: 0

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Previous	NASA TN D-3825 CRACK PROPAGATION, DELAYED FAILURE, AND RESIDUAL STATIC STRENGHT OF TITANIUM, ALUMINIUM, AND STAINLESS STEEL ALLOYS IN AQUEOUS ENVIRONMENTS	NASA TN D-3826 ECCENTRICALLY STIFFENED SHALLOW SHELLS OF DOUBLE CURVATURE	NASA TN D-3827 Aerodynamic characteristics at mach 2.03 of a series of curved-leading-edge wings employing various degrees of twist and camber	NASA TN D-3828 OPERATIONAL FEATURES OF THE LANGLEY LUNAR LANDING RESEARCH FACILITY	NASA TN D-3829 EFFECT OF ORIFICE SIZE AND HEAT-TRANSFER RATE ON MEASURED STATIC PRESSURE IN A LOW-DENSITY ARC-HEATED WIND TUNNEL	NASA TN D-3830 FLIGHT DEMONSTRATION OF A SKIN-FRICTION GAGE TO A LOCAL MACH NUMBER OF 4.9	NASA TN D-3832 ROLLING-ELEMENT FATIGUE LIFE OF SAE 52100 STEEL HOLLOW BALLS	Next

Bound With Nasa Tn D-3821-27,3829-30

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