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Welcome to P K Kelkar Library, Online Public Access Catalogue (OPAC)

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1.
Performance and stability characteristics of nitrogen tetroxide-hydrazine combustors [NASA TN D-4776]

by Hersch, Martin.

Material type: book Book; Format: print ; Literary form: not fiction Description: 20p.Publisher: Washington, D.C. Nasa 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4776] (1).

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2.
STUDY OF HELIUM PENETRATION AND SPREDING IN A MACH 2 AIRSTREAM USING A DELTA WING INJECTOR

by Povinelli,Louis A, Povinelli,Frederick P | Hersch,Martin.

Material type: book Book Description: 15.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5322 -] (1).

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3.
OPTICAL STUDY OF SONIC AND SUPERSONIC JET PENETRATION FROM A FLAT PLATE INTO A MACH 2 AIRSTREAM

by Hersch,Martin,Povinelli,Louis A | Povinelli,Frederick P.

Material type: book Book Description: 13.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5717] (1).

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4.
EFFECT OF INERCHANGING PROPELLANTS ON ROCKET COMBUSTOR PERFORMANCE WITH COAXIAL INJECTION.

by Hersch,Martin.

Material type: book Book Description: 21.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2369] (1).

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5.
HYDROGEN-OXYGEN CHEMICAL REACTION KINETICS IN ROCKET ENGINE COMBUSTION

by Hersch,Martin.

Material type: book Book Description: 17.Publisher: Nasa, Washington, D.C. 1967Availability: No items available Damaged (1).

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6.
COMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO

by Hersch,Martin.

Material type: book Book Description: 13.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-129] (1).

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7.
A mixing model for rocket engine combustion [NASA TN D-2881]

by Hersch, Martin.

Material type: book Book; Format: print ; Literary form: not fiction Description: 24p.Publisher: Washington, D. C. NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2881] (1).

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