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NASA TN [D-7673] : CREEP BEHAVIOR OF TANTALUM ALLOY T-222 AT 1365 TO 1700K

By: Titran,Robert H.

Series: NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1974Description: 31p.Subject(s): Aeronautics

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-7673	Not for loan		TR7468

Total holds: 0

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Previous	Introduction to computer-aided reliability data analysis [ NAS TN D-5009]	Tensile properties and creep strength of three aluminium alloys exposed upto 25000 hours at 200 degree to 400 degree F (370 degree to 480 degree K) [NASA TN D-5010]	NASA TN [D-7672]	NASA TN [D-7673]	NASA Technical Note [NASA TN D-3022]: Evaluation of the lateral-directional stability and control characteristics of the lightweight M2-F1 lifting body at low speed	NASA Technical Note [NASA TN D-3023]: Design and operational characteristics of a lunar-landing research vehicle	NASA Technical Note [NASA TN D-3024]: Design and overall performance of an axial-flow pump rotor with a blade-tip diffusion factor of 0.66	Next

NASA Technical Note D-7671-7680
Bounded Volumes Accession No.102517; Contents: TR7467-7475

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