Normal view MARC view ISBD view

STATIC AERODYNAMIC CHARACTERISTICS OF A TWO-STAGE AND A THREE -STAGE ROCKET VEHICLE AT MACH NUMBERS FROM 1.47 TO 4.63

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1962Description: 79.DDC classification: NASA | TN D-1232

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-1232 (Browse shelf)	Not for loan		TR13001

Total holds: 0

Previous								Next
Previous	NASA TN D-1229 HUMAN PILOT' DYNAMIC-RESPONSE CHARACTERISTICS MEASURED IN FLIGHT AND ON A NONMOVING SIMULATOR	NASA TN D-123 INVESTIGATION OF THE EFFECT OF A GUIDE-VANE-ROTOR COMBINATION ON INLET TOTAL-PRESSURE DISTORTION IN A COMPRESSIBLE FLUID	NASA TN D-1230 ANALYSIS OF TWO THRUSTING TECHNIQUES FOR SOFT LUNAR LANDINGS STARTING FROM A 50-MILE ALTITUDE CIRCULAR ORBIT	NASA TN D-1232 STATIC AERODYNAMIC CHARACTERISTICS OF A TWO-STAGE AND A THREE -STAGE ROCKET VEHICLE AT MACH NUMBERS FROM 1.47 TO 4.63	NASA TN D-1233 EFFECTS OF COUPLING BETWEEN PITCH AND ROLL CONTROL INPUTS ON THE HANDLING QUALITIES OF VTOL AIRCRAFT	NASA TN D-1234 FORCE-TEST INVESTIGATION OF A MODEL OF AN AERIAL VEHICLE SUPPORTED BY FOUR UNSHROUDED PROPELLERS	NASA TN D-1235 FLIGHT-TEST INVESTIGATION OF A MODEL OF AN AERIAL VEHICLE SUPPORTED BY FOUR UNSHROUDED PROPELLERS	Next

Bound With Nasa Tn D-1231,1233-1240

There are no comments for this item.

PKK Library