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Hypervelocity impact damage characteristics in armored space radiator tubes

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Material type: Text

TextLanguage: English Series: National Aeronautics Space AgencyPublication details: Washington, D. C. NASADescription: 42pDDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA TN- 2472 (Browse shelf(Opens below))	Not for loan		83668A

Total holds: 0

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Previous	NASA CR-2044 APPLICATIONS OF THE THEORY OF OPTIMAL CONTROL OF DISTRIBUTED-PARAMETER SYSTEMS TO STRUCTURAL OPTIMIZATION[NASA CR-2044]	NASA CR-2045 EVALUATION OF INSULATION MATERIALS AND COMPOSITES FOR USE IN A NUCLEAR RADIATION ENVIRONMENT, PHASE I [NASA CR-2045]	NASA TM X-606 Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24o swept wing [NASA TM X-606]	NASA TN- 2472 Hypervelocity impact damage characteristics in armored space radiator tubes	NASA TN D-1281 Analytical and experimental investigation of forces and frequencies resulting from liquid [NASA TN D-1281]	NASA TN D-1525 Influence of weight parameters on the propulsion requirements of orbit-launched vehicles [NASA TN D-1525]	NASA TN D-2471 The equilibrium free surface of contained liquid under low gravity and centrifugal forces	Next

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