Development of a protective coating system for regeneratively cooled thrust chambers Final technical report, 1 Jul. 1967 - 31 Mar. 1969

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 a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report

Stubbs, V. R.

May 1969

Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engin

Research and development program on magnetic, electrical conductor, electrical insulation, and bore seal materials Final report, Aug. 1963 - Dec. 1964

Kueser, P. E.

January 1965

Magnetic, electric conductor, electric insulation, and bore seal materials for advanced space electr...

Protective coating system for a regeneratively cooled thrust chamber Final report, 1 Feb. 1969 - 31 Dec. 1970

Carpenter, H. W.

June 1971

Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber

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

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...

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

Space storable thruster investigation

Campbell, J. G.

October 1971

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

Liquid propellant thermal conditioning system Interim report

Sterbentz, W. H.

April 1967

Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas

Development of protective coatings for chromium-base alloys Semiannual progress report

English, J. J.
Mac Millan, C. A.
Bartlett, E. S.
Williams, D. N.

July 1966

Feasibility of using ductile nickel-chromium alloy claddings to protect chromium alloy turbine vanes...

Thermal performance of multilayer insulations Final report

Keller, C. W.

April 1971

Composite multilayer insulation system of double goldized, Nylar radiation shield

Development of thermal radiative surface coatings for nasa-lewis space simulation chamber final report, 29 jun. - 30 may 1965

Baldrige, J. H.

January 1965

Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...

Activation and Initial Test Operations, Large Rocket Engine - Thrust Chamber Test Facilities Technology Report

Clark, D. H.

August 1967

Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin

Advanced refractory alloy corrosion loop program Quarterly progress report no. 4, Jan. 15 - Apr. 15, 1966

Harrison, R. W.

April 1966

Refractory alloy materials procurement and evaluation for potassium corrosion loop progra

Liquid propellant thermal conditioning system Final report

Sterbentz, W. H.

August 1968

Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan

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 a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report

Stubbs, V. R.

May 1969

Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engin

Research and development program on magnetic, electrical conductor, electrical insulation, and bore seal materials Final report, Aug. 1963 - Dec. 1964

Kueser, P. E.

January 1965

Magnetic, electric conductor, electric insulation, and bore seal materials for advanced space electr...

Protective coating system for a regeneratively cooled thrust chamber Final report, 1 Feb. 1969 - 31 Dec. 1970

Carpenter, H. W.

June 1971

Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber

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

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...

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

Space storable thruster investigation

Campbell, J. G.

October 1971

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

Liquid propellant thermal conditioning system Interim report

Sterbentz, W. H.

April 1967

Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas

Development of protective coatings for chromium-base alloys Semiannual progress report

English, J. J.
Mac Millan, C. A.
Bartlett, E. S.
Williams, D. N.

July 1966

Feasibility of using ductile nickel-chromium alloy claddings to protect chromium alloy turbine vanes...

Thermal performance of multilayer insulations Final report

Keller, C. W.

April 1971

Composite multilayer insulation system of double goldized, Nylar radiation shield

Development of thermal radiative surface coatings for nasa-lewis space simulation chamber final report, 29 jun. - 30 may 1965

Baldrige, J. H.

January 1965

Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...

Activation and Initial Test Operations, Large Rocket Engine - Thrust Chamber Test Facilities Technology Report

Clark, D. H.

August 1967

Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin

Advanced refractory alloy corrosion loop program Quarterly progress report no. 4, Jan. 15 - Apr. 15, 1966

Harrison, R. W.

April 1966

Refractory alloy materials procurement and evaluation for potassium corrosion loop progra

Liquid propellant thermal conditioning system Final report

Sterbentz, W. H.

August 1968

Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan

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 a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report

Stubbs, V. R.

May 1969

Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engin

Research and development program on magnetic, electrical conductor, electrical insulation, and bore seal materials Final report, Aug. 1963 - Dec. 1964

Kueser, P. E.

January 1965

Magnetic, electric conductor, electric insulation, and bore seal materials for advanced space electr...

Development of a protective coating system for regeneratively cooled thrust chambers Final technical report, 1 Jul. 1967 - 31 Mar. 1969

Abstract

Extracted data

Development of a protective coating system for regeneratively cooled thrust chambers Final technical report, 1 Jul. 1967 - 31 Mar. 1969

Abstract

Extracted data

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