Investigation of advanced regenerative thrust chamber designs Final report

Fluorine-hydrogen performance evaluation. Phase I, part I - Analysis, design, and demonstration of high performance injectors for the liquid fluorine-gaseous hydrogen combination Final report

Clapp, S. D.
Arbit, H. A.

August 1966

Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...

Space storable regenerative cooling investigation Interim report, 1 Jul. - 30 Sep. 1967

Mitchell, J. P.

July 1968

Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer

Regeneratively cooled rocket engine for space storable propellants

Wagner, W. R.

July 1973

Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...

Space storable regenerative cooling investigation Final report, Jul. 1967 - May 1970

Pauckert, R. P.

June 1970

Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...

Development of advanced fabrication techniques for regeneratively cooled thrust chambers by the electroforming process Final report

Hammer, S.
Czacka, Z.

October 1967

Fabrication techniques for regeneratively cooled thrust chambers by electroforming proces

Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure

Manning, F. L. C.
Curren, A. N.
Krueger, R. C.
Price, H. G., Jr.

September 1967

Heat-transfer rates and coefficients and coolant pressure loss characteristics in regeneratively coo...

Performance of a transpiration-regenerative cooled rocket thrust chamber

Valler, H. W.

September 1979

The analysis, design, fabrication, and testing of a liquid rocket engine thrust chamber which is gas...

Investigation of light hydrocarbon fuels with fluorine oxygen mixtures as liquid rocket propellants Final report

Masters, A. I.

November 1968

Analytical and experimental study of regenerative cooling for FLOX methane engine with bulk boiling ...

Coatings for regenerative engines /follow-up program/ Final report, 1 Jul. 1968 - 30 Jan. 1970

Lewis, W. J.

July 1970

Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...

Investigation of thrusters for cryogenic reaction control systems, volume 1 Final report, Jun. 1968 - Oct. 1969

Johnson, R. J.

November 1970

Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...

Protective coating system for a regeneratively cooled thrust chamber Final report, 30 Jun. 1967 - 31 Jan. 1969

Carpenter, H. W.

February 1969

Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe

Development of advanced fabrication techniques for regeneratively cooled thrust chambers by the gas-pressure-bonding process Final report, 29 Jun. 1967 - 30 Apr. 1970

Ryan, M. J.
Goldstein, M.
Ashurst, A. N.

October 1970

Production of regeneratively cooled rocket thrust chambers by removable tooling and subsequent hot i...

Space storable regenerative cooling investigation Interim report, Jul. - Dec. 1967

Pauckert, R. P.

September 1968

Regenerative cooling capabilities of light hydrocarbon fuels used with FLOX and oxygen fluoride

Space storable thruster investigation

Campbell, J. G.

October 1971

Design, characteristics, and test firing of radiation and film cooled 25 pound thrust graphitic thru...

Space storable thrustor investigation Final report

Fiorito, R. J.
Coulbert, C. D.

June 1969

Design and performance of space storable liquid FLOX methane thrustor of refractory composite materi...

Fluorine-hydrogen performance evaluation. Phase I, part I - Analysis, design, and demonstration of high performance injectors for the liquid fluorine-gaseous hydrogen combination Final report

Clapp, S. D.
Arbit, H. A.

August 1966

Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...

Space storable regenerative cooling investigation Interim report, 1 Jul. - 30 Sep. 1967

Mitchell, J. P.

July 1968

Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer

Regeneratively cooled rocket engine for space storable propellants

Wagner, W. R.

July 1973

Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...

Space storable regenerative cooling investigation Final report, Jul. 1967 - May 1970

Pauckert, R. P.

June 1970

Analysis to determine regenerative cooling limits of light hydrocarbons used with FLOX and OF2 over ...

Development of advanced fabrication techniques for regeneratively cooled thrust chambers by the electroforming process Final report

Hammer, S.
Czacka, Z.

October 1967

Fabrication techniques for regeneratively cooled thrust chambers by electroforming proces

Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure

Manning, F. L. C.
Curren, A. N.
Krueger, R. C.
Price, H. G., Jr.

September 1967

Heat-transfer rates and coefficients and coolant pressure loss characteristics in regeneratively coo...

Performance of a transpiration-regenerative cooled rocket thrust chamber

Valler, H. W.

September 1979

The analysis, design, fabrication, and testing of a liquid rocket engine thrust chamber which is gas...

Investigation of light hydrocarbon fuels with fluorine oxygen mixtures as liquid rocket propellants Final report

Masters, A. I.

November 1968

Analytical and experimental study of regenerative cooling for FLOX methane engine with bulk boiling ...

Coatings for regenerative engines /follow-up program/ Final report, 1 Jul. 1968 - 30 Jan. 1970

Lewis, W. J.

July 1970

Testing thermal barrier coatings for flame surface of regeneratively cooled chamber operating with F...

Investigation of thrusters for cryogenic reaction control systems, volume 1 Final report, Jun. 1968 - Oct. 1969

Johnson, R. J.

November 1970

Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...

Protective coating system for a regeneratively cooled thrust chamber Final report, 30 Jun. 1967 - 31 Jan. 1969

Carpenter, H. W.

February 1969

Ceramic thermal protective coating system for regeneratively cooled hydrogen oxygen thrust chambe

Development of advanced fabrication techniques for regeneratively cooled thrust chambers by the gas-pressure-bonding process Final report, 29 Jun. 1967 - 30 Apr. 1970

Ryan, M. J.
Goldstein, M.
Ashurst, A. N.

October 1970

Production of regeneratively cooled rocket thrust chambers by removable tooling and subsequent hot i...

Space storable regenerative cooling investigation Interim report, Jul. - Dec. 1967

Pauckert, R. P.

September 1968

Regenerative cooling capabilities of light hydrocarbon fuels used with FLOX and oxygen fluoride

Space storable thruster investigation

Campbell, J. G.

October 1971

Design, characteristics, and test firing of radiation and film cooled 25 pound thrust graphitic thru...

Space storable thrustor investigation Final report

Fiorito, R. J.
Coulbert, C. D.

June 1969

Design and performance of space storable liquid FLOX methane thrustor of refractory composite materi...

Fluorine-hydrogen performance evaluation. Phase I, part I - Analysis, design, and demonstration of high performance injectors for the liquid fluorine-gaseous hydrogen combination Final report

Clapp, S. D.
Arbit, H. A.

August 1966

Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...

Space storable regenerative cooling investigation Interim report, 1 Jul. - 30 Sep. 1967

Mitchell, J. P.

July 1968

Regenerative cooling capabilities of light hydrocarbon fuels when used with fluorinated oxidizer

Regeneratively cooled rocket engine for space storable propellants

Wagner, W. R.

July 1973

Analysis, design, fabrication, and test efforts were performed for the existing OF2/B2H6 regenerativ...

Investigation of advanced regenerative thrust chamber designs Final report

Abstract

Extracted data

Investigation of advanced regenerative thrust chamber designs Final report

Abstract

Extracted data

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