Normal view MARC view ISBD view

EFFECTS OF CONTROL-RESPONSE CHARACTERISTICS ON THE CAPABILITY OF HELICOPTER FOR USE AS A GUN PLATEFORM

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1960Description: 17.DDC classification: NASA | TN D-464

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-464 (Browse shelf)	Not for loan		TR13493

Total holds: 0

Previous								Next
Previous	NASA TN D-463 MEASUREMENT OF THE ERRORS OF SERVICE ALTIMETER INSTALLATIONS DURING LANDING-APPROCH AND TAKE-OFF OPERATIONS	NASA TN D-4630 - FRICTION AND WEAR UNDER FRETTING CONDITIONS OF MATERIALS FOR USE AS WIRE FRICTION DAMPERS OF COMPRESSOR BLADE VIBRATION	NASA TN D-4638 SIMULATION STUDIES OF THE SUPERSONIC TRANSPORT IN THE PRESENT-DAY AIR TRAFFIC CONTROL SYSTEM.	NASA TN D-464 EFFECTS OF CONTROL-RESPONSE CHARACTERISTICS ON THE CAPABILITY OF HELICOPTER FOR USE AS A GUN PLATEFORM	NASA TN D-4641 - A TECHNIQUE FOR PASSIVE ATTITUDE CONTROL 0F SOLAR ORIENTED INTERPLANETARY SPACECRAFT	NASA TN D-465 THE MAGNETIC FIELD OF A FINITE SOLENOID	NASA TN D-466 A GRAPHICAL METHOD FOR ESTIMATING ION-ROCKET PERFORMANCE	Next

Bound With Nasa Tn D-461-63,465-69

There are no comments for this item.

PKK Library