Normal view MARC view ISBD view

EFFECTS OF FLANK LOSSES IN THE THEORY OF SPACE-PROBE ENTRY UNDER CONDITIONS OF HIGH MASS LOSS.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1963Description: 37.DDC classification: NASA | TN D-2050

average rating: 0.0 (0 votes)

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-2050 (Browse shelf)	Not for loan Untraceable		TR11953

Total holds: 0

Previous								Next
Previous	NASA TN D-2048 BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01	NASA TN D-2049 FEASIBILITY STUDY OF A BANG-BANG PATH CONTROL FOR A REENTRY VEHICLE.	NASA TN D-205 FREE-FLIGHT INVESTIGATION AT MACH NUMBERS BETWEEN 0.5 AND 1.7 OF THE ZERO-LIFT ROLLING EFFECTIVENESS AND DRAG OF VARIOUS SURFACE, SPOILER, AND JET CONTROLS ON AN 80(DEGRE) DELTA-WING MISSILE	NASA TN D-2050 EFFECTS OF FLANK LOSSES IN THE THEORY OF SPACE-PROBE ENTRY UNDER CONDITIONS OF HIGH MASS LOSS.	NASA TN D-2052 THE DESIGN OF SAILPLANES FOR OPTIMUM THERMAL SOARING PERFORMANCE.	NASA TN D-2053 WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.	NASA TN D-2055 STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.	Next

Bound With Nasa Tn D-2041-49

There are no comments for this item.

PKK Library