Injector orifice study, Apollo service propulsion system Summary report, 7 Apr. 1967 - 31 Jul. 1968

Space shuttle auxiliary propulsion system design study

Kelly, P. J.

August 1971

Development of requirements for auxilary propulsion system used with baseline orbiter and booster of...

Apollo experience report: Ascent propulsion system

Humphries, C. E.
Taylor, R. E.

March 1973

The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...

Apollo 15 mission report. Supplement 2: Service propulsion system final flight evaluation

Wood, S. C.
Smith, R. J.

November 1972

The command and service module 112 service propulsion system performance for the Apollo 15 mission w...

Apollo service propulsion system rocket engine bipropellant valve improvement program Final report

February 1971

Rocket engine bipropellant valve improvement for Apollo service propulsion syste

Apollo RCS positive expulsion tankage product improvement program. Task F - Integration and verification of solutions Final report, Jul. 1967 - Sep. 1969

January 1970

Environmental tests of design modifications for Apollo RCS positive expulsion tankag

Planning research in the area of launch vehicle and propulsion programs Progress report, 1-31 Mar. 1968

Weller, A. E.
Davis, B. W.
Nippert, D. A.
Porter, R. F.
Edgecombe, D. S.

April 1968

Program and report reviews on launch vehicle upper stages and propulsion of advanced reentry spacecr...

Apollo experience report: Service propulsion subsystem

Wood, J. A.
Gibson, C. R.

August 1973

The significant service propulsion subsystem development, qualification, and flight experience from ...

Sterilizable liquid propulsion system Quarterly progress report, 2 Jan. - 31 Mar. 1967

Brady, H. F.
Holt, C.

April 1967

Basic design, component selection, and materials compatibility tests for sterilizable liquid biprope...

Advanced injector concepts investigation Final summary report

April 1971

Evaluation of throttling injector concepts applicable to advanced cryogenic engine

Noncircular orifice holes and advanced fabrication techniques for liquid rocket injectors. Phase 2 - Analytical and experimental study of noncircular injector orifices, and elements for gas/liquid injectors Final report

Mc Hale, R. M.

February 1971

Characteristics of noncircular injector orifices and elements for gas and liquid injector

Apollo experience report: Thermal protection from engine-plume environments

Taylor, J. T.

June 1972

Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...

Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 2

Kerkam, B. F.
Wood, A. A.
Foley, M. G.
Smith, D. W.

January 1969

Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion ...

Advanced injector concepts investigation Final report

April 1971

Liquid propellant rocket engine throttling injector design based on exhaust gas counter flow and hea...

Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1

Kerkam, B. F.
Foley, M. G.
Smith, D. W.
Wood, A. A.

January 1969

Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsio...

Results of a space shuttle pulme impingement investigation at stage separation in the NASA-MSFC impulse base flow facility

Sims, W. H.
Mccanna, R. W.

July 1972

Results are presented for an experimental space shuttle stage separation plume impingement program c...

Space shuttle auxiliary propulsion system design study

Kelly, P. J.

August 1971

Development of requirements for auxilary propulsion system used with baseline orbiter and booster of...

Apollo experience report: Ascent propulsion system

Humphries, C. E.
Taylor, R. E.

March 1973

The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...

Apollo 15 mission report. Supplement 2: Service propulsion system final flight evaluation

Wood, S. C.
Smith, R. J.

November 1972

The command and service module 112 service propulsion system performance for the Apollo 15 mission w...

Apollo service propulsion system rocket engine bipropellant valve improvement program Final report

February 1971

Rocket engine bipropellant valve improvement for Apollo service propulsion syste

Apollo RCS positive expulsion tankage product improvement program. Task F - Integration and verification of solutions Final report, Jul. 1967 - Sep. 1969

January 1970

Environmental tests of design modifications for Apollo RCS positive expulsion tankag

Planning research in the area of launch vehicle and propulsion programs Progress report, 1-31 Mar. 1968

Weller, A. E.
Davis, B. W.
Nippert, D. A.
Porter, R. F.
Edgecombe, D. S.

April 1968

Program and report reviews on launch vehicle upper stages and propulsion of advanced reentry spacecr...

Apollo experience report: Service propulsion subsystem

Wood, J. A.
Gibson, C. R.

August 1973

The significant service propulsion subsystem development, qualification, and flight experience from ...

Sterilizable liquid propulsion system Quarterly progress report, 2 Jan. - 31 Mar. 1967

Brady, H. F.
Holt, C.

April 1967

Basic design, component selection, and materials compatibility tests for sterilizable liquid biprope...

Advanced injector concepts investigation Final summary report

April 1971

Evaluation of throttling injector concepts applicable to advanced cryogenic engine

Noncircular orifice holes and advanced fabrication techniques for liquid rocket injectors. Phase 2 - Analytical and experimental study of noncircular injector orifices, and elements for gas/liquid injectors Final report

Mc Hale, R. M.

February 1971

Characteristics of noncircular injector orifices and elements for gas and liquid injector

Apollo experience report: Thermal protection from engine-plume environments

Taylor, J. T.

June 1972

Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...

Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 2

Kerkam, B. F.
Wood, A. A.
Foley, M. G.
Smith, D. W.

January 1969

Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion ...

Advanced injector concepts investigation Final report

April 1971

Liquid propellant rocket engine throttling injector design based on exhaust gas counter flow and hea...

Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1

Kerkam, B. F.
Foley, M. G.
Smith, D. W.
Wood, A. A.

January 1969

Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsio...

Results of a space shuttle pulme impingement investigation at stage separation in the NASA-MSFC impulse base flow facility

Sims, W. H.
Mccanna, R. W.

July 1972

Results are presented for an experimental space shuttle stage separation plume impingement program c...

Space shuttle auxiliary propulsion system design study

Kelly, P. J.

August 1971

Development of requirements for auxilary propulsion system used with baseline orbiter and booster of...

Apollo experience report: Ascent propulsion system

Humphries, C. E.
Taylor, R. E.

March 1973

The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...

Apollo 15 mission report. Supplement 2: Service propulsion system final flight evaluation

Wood, S. C.
Smith, R. J.

November 1972

The command and service module 112 service propulsion system performance for the Apollo 15 mission w...

Injector orifice study, Apollo service propulsion system Summary report, 7 Apr. 1967 - 31 Jul. 1968

Abstract

Extracted data

Injector orifice study, Apollo service propulsion system Summary report, 7 Apr. 1967 - 31 Jul. 1968

Abstract

Extracted data

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