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DEVELOPMENT AND TESTING OF THE DISK-GAP-BAND PARACHUTE USED FOR LOW DYNAMIC PRESSURE APPLICATIONS AT EJECTION ALTITUDES AT OR ABOVE 200,000 FEET

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BookPublisher: Nasa, Washington, D.C. 1966Description: VII,57.DDC classification: NASA | CR-502 -

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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 CR-502 - (Browse shelf)	Not for loan		TR8349

Total holds: 0

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Previous	NASA CR-498 OPTICAL-INERTIA SPACE SEXTANT FOR AN ADVANCED SPACE NAVIGATION SYSTEM. PHASE B	NASA CR-499 APPLICATIONS OF THE CALCULUS OF VARIATIONS TO AIRCRAFT PERFORMANCE.	NASA CR-500 DESIGN CONSIDERACTIONS FOR THERMOSTATIC FIN SPACECRAFT TEMPERATURE CONTROL.	NASA CR-502 - DEVELOPMENT AND TESTING OF THE DISK-GAP-BAND PARACHUTE USED FOR LOW DYNAMIC PRESSURE APPLICATIONS AT EJECTION ALTITUDES AT OR ABOVE 200,000 FEET	NASA CR-503 - DESIGN STUDIES OF ADVANCED LENTICULAR PASSIVE COMMUNICATION SATELLITES FROM LOW TO SYNCHRONOUS ORBIT	NASA CR-504 - VIBROCARDIOGRAPHIC SYSTEM STUDY	NASA CR-505 - STUDIES IN PRESTRESSED AND SEGMENTED BRITTLE STRUCTURES	Next

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