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NASA ENGINEERING MODELS OF THE MARS ATMOSPHERE FOR ENTRY VEHICLE DESIGN

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BookPublisher: Nasa, Washington, D.C. 1964Description: 47.DDC classification: NASA | TN D-2525

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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-2525 (Browse shelf)	Not for loan		TR16213

Total holds: 0

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Previous	NASA TN D-2493 - EVALUATION OF SELECTED ERFRACTORY OXIDE MATERIALS FOR USE IN HIGH-TEMPERATURE PEBBLE-BED WIND-TUNNEL HEAT EXCHANGERS	NASA TN D-2496 - REAL-GAS INVISCID NOZZLE CONTOURS FOR NITROGEN AT MACH 15, 17, AND 19 WITH TABULATED PROPERTIES FOR THE CALCULATION OF BOUNDARY-LAYER EFFECTS	NASA TN D-25 - Large-scale wind-tunnel tests of an airplane model with an unswept ,aspect-ratio-10 wing,four propellers ,and blowing flaps	NASA TN D-2525 NASA ENGINEERING MODELS OF THE MARS ATMOSPHERE FOR ENTRY VEHICLE DESIGN	NASA TN D-2552 LARGE-SCALE WIND-TUNNEL TESTS ON AN ASPECT RATIO 2.17 DELTA-WING MODEL EQUIPPED WITH MIDCHORD BOUNDARY-LAYER-CONTROL FLAPS.	NASA TN D-2553 PERFORMANCE OF 84 DEGREE FLAT-PLATE HELICAL INDUCER AND COMPARISON WITH PERFORMANCE OF SIMILAR 78 DEGREE AND 80.6 DEGREE INDUCERS.	NASA TN D-2554 MAGNETIC BREAKDOWN IN A FINITE ONE-DIMENSIONAL MODEL.	Next

Bound With Nasa Tn D-2521-2524,2526-2530

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