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NASA Technical Note [NASA TN D-4674]: Hot-salt-stress-corrosion cracking and its effect on tensile properties of Ti-8Al-1Mo-1V titanium-alloy sheet
by Washington. National Aeronautics and Space Administration (NASA) Dick M. Royster | Royster, Dick M. Material type:  Book Description: 34p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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2.
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INVESTIGATION OF MECHANICAL PROPERTIES AND METALLURGICAL CHARACTERISTICS OF A METALLIC CHROMIUM AND MAGNESIUM OXIDE COMPOSITE
by Manning,Charles R | Royster,Dick M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 44p.Publisher: NASA, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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NASA Technical Note [NASA TN D-1944]: An investigation of a new nickel alloy strengthened by dispersed thoria
by Washington. National Aeronautics and Space Administration (NASA) | Manning, Charles R | Royster, Dick M | Braski, David N. Material type: Book Description: 38p.Publisher: Washington NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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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]
by Royster, Dick M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 42p.Publisher: Washington, D.C. NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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EFFECTS OF LONGTIME ENVIRONMENTAL EXPOSURE ON MECHANICAL PROPERTIES OF SHEET MATERIALS FOR A SUPERSONIC TRANSPORT.
by Pride,Richard A,Royster,Dick M | A. Material type: Book Description: 23.Publisher: National Aeronautics And Space Administration, Washington, D.C. Availability: No items available Damaged (1).
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6.
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EFFECT OF HIGH-TEMPERATURE CREEP AND OXIDATION ON RESIDUAL ROOM-TEMPERATURE PROPERTIES FOR SEVERAL THIN-SHEET SUPERALLOYS
by Royster,Dick M | Lisagor,W Barry. Material type: Book Description: 118.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6893] (1).
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7.
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NASA TN [D-5417]
: HOT-SALT-STRESS-CORROSION CRACKING AND ITS EFFECT ON TENSILE AND STRESS-RUPTURE PROPERTIES OF TI-6A1-4V TITANIUM-ALLOY SHEET
by Royster, Dick M. Description: 35p.Publisher: NASA, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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DESIGN, TESTS, AND ANALYSIS OF A HOT STRUCTURE FOR LIFTING REENTRY VEHICLES
by Pride,Richard A,Royster,Dick M | Helms,Bobbie F. Material type: Book Description: 149.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2186] (1).
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9.
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EXPERIMENTAL STUDY OF A HOT STRUCTURE FOR A REENTRY VEHICLE
by Pride,Richard A,Royster,Dick M | Helms,Bobbie F. Material type: Book Description: 13.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-314] (1).
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10.
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NASA TN [D-5670]
: Influence of salt and levated temperature exposure on the maxmum compressive strength of titanium alloy skin-stringer panels
by Gardner, James E | Royster, Dick M. Description: 32p.Publisher: Washington National Aeronautics and Space Administration 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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