Normal view MARC view ISBD view

WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1964Description: 81.DDC classification: NASA | TN D-2053

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-2053 (Browse shelf)	Not for loan		TR15577

Total holds: 0

Previous								Next
Previous	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.	NASA TN D-2056 PHENOMENA OF PNEUMATIC TIRE HYDROPLANNING.	NASA TN D-2057 STATIC LONGITUDINAL CHRACTERISTICS OF THE PROJECT FIRE REENTRY STAGE AFTER REENTRY-PACKAGE SEPRATION AT MACH 28.3 IN HELIUM.	Next

Bound With Nasa Tn D-2051-2052,2054-2060.

There are no comments for this item.

PKK Library