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THEORETICAL PERFORMANCE OF HYDROGEN-OXYGEN ROCKET THRUST CHAMBERS

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BookPublisher: Nasa, Washington, D.C. 1961Description: 75.DDC classification: NASA | TR R-111

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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 TR R-111 (Browse shelf)	Not for loan		65630

Total holds: 0

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Previous	NASA TR R-108 MEASUREMENTS OF THE DISSOCIATION RATE OF MOLECULAR OXYGEN	NASA TR R-109 HYPERSONIC VISCOUS SHOCK LAYER OF NONEQUILIBRIUM DISSOCIATING GAS	NASA TR R-110 ANALYTICAL METHOD OF APPROXIMATING THE MOTION OF A SPINNING VEHICLE WITH VARIABLE MASS AND INERTIA PROPERTIES ACTED UPON BY SEVERAL DISTURBING PARAMETERS	NASA TR R-111 THEORETICAL PERFORMANCE OF HYDROGEN-OXYGEN ROCKET THRUST CHAMBERS	NASA TR R-112 A METHOD FOR THE CALCULATION OF LATTICE ENERGIES OF COMPLEX CRYSTALS WITH APPLICATION TO THE OXIDES OF MOLYBDENUM	NASA TR R-113 STUDY OF STATISTICAL DATA-ADJUSTMENT AND LOGIC TECHNIQUES AS APPLIED TO THE ITERPLANETARY MIDCOURSE GUIDANCE PROBLEM	NASA TR R-114 A THEORETICAL TREATMENT OF THE STEADY-FLOW,LINEAR,CROSSED-FIELD,DIRECT-CURRENT PLASMA ACCELERATOR FOR INVISCID,ADIABATIC,ISOTHERMAL, CONSTANT-AREA FLOW	Next

Bound With Nasa Tr R-112-20

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