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ANALYSIS OF LARGE BENDING DEFORMATIONS OF A FILAMENTARY TUBULAR SHELL TYPICAL FOR PRESSURE CONSTRANT COMPONENTS OF SPACE SUITS.

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BookPublisher: Nasa, Washington, D.C. 1970Description: 47.DDC classification: NASA | CR-1507

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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-1507 (Browse shelf)	Not for loan		TR11534

Total holds: 0

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Previous	NASA CR-1503 AN APPLICATION OF THE REQUIREMENT VS CAPABILITY ANALYSIS TO ESTIMATING DESIGN RELIABILITY OF SOLID ROCKET MOTORS.	NASA CR-1504 MEASUREMENTS OF THE EXTINCTION PARAMETERS OF HOT SEEDED HYDROGEN AT 1-ATMOSPHERE PRESSURE.	NASA CR-1505 THEORETICAL CALCULATIONS OF PARTICLE-SEEDED GASES.	NASA CR-1507 ANALYSIS OF LARGE BENDING DEFORMATIONS OF A FILAMENTARY TUBULAR SHELL TYPICAL FOR PRESSURE CONSTRANT COMPONENTS OF SPACE SUITS.	NASA CR-1508 RESEARCHESIN OPTIMAL RENDEZVOUS.	NASA CR-1509 CB-1ZR RANKINE SYSTEM CORROISON TEST LOOP.	NASA CR-1510 A PROCEDURE FOR ASSESSING AIRCRAFT TURBULENCE-PENETRATION PERFORMANCE.	Next

Bound With Nasa Cr-1506,1508-10.

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