National Technical Reports Library

The National Technical Information Service acquires, indexes, abstracts, and archives the largest collection of U.S. government-sponsored technical reports in existence. The NTRL offers online, free and open access to these authenticated government technical reports. Technical reports and documents in its repository may be available online for free either from the issuing federal agency, the U.S. Government Publishing Office’s Federal Digital System website, or through search engines.

Details

Air Force Reusable Rocket Engine Program XLR129-P-1 Engine Performance.

AD500578

Publication Date	1969
Personal Author	Atherton, R. R.
Page Count	82
Abstract	This special technical report presents information and data on the XLR129-P-1 rocket engine. Information is presented for both the demonstrator engine and flight engine versions of this rocket engine. A general description and pertinent technical information are presented for the demonstrator engine. The demonstrator engine program schedule is also presented. Parametric design, performance, cost, and schedule data are presented for the flight engine. This technical report has been prepared for the use of airframe manufacturers and government personnel who are conducting mission and vehicle studies. (Author)
Keywords	Recoverable booster motors Liquid propellant rocket engines Liquid rocket propellants Liquid rocket oxidizers Liquid rocket fuels Design Performance(Engineering) Lr-129 engines Xlr-129-p-1 engines Cooling Transpiration Underexpanded nozzle flow
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	81G - Rocket Engines & Motors 81H - Rocket Propellants
Corporate Authors	Pratt and Whitney Aircraft, West Palm Beach, FL. Florida Research and Development Center.
Document Type	Technical Report
Title Note	Special rept.
NTIS Issue Number	198615
Contract Number	F04611-68-C-0002

Air Force Reusable Rocket Engine Program XLR129-P-1 Engine Performance.

Air Force Reusable Rocket Engine Program XLR129-P-1 Engine Performance.
AD500578

Publication Date	1969
Personal Author	Atherton, R. R.
Page Count	82
Abstract	This special technical report presents information and data on the XLR129-P-1 rocket engine. Information is presented for both the demonstrator engine and flight engine versions of this rocket engine. A general description and pertinent technical information are presented for the demonstrator engine. The demonstrator engine program schedule is also presented. Parametric design, performance, cost, and schedule data are presented for the flight engine. This technical report has been prepared for the use of airframe manufacturers and government personnel who are conducting mission and vehicle studies. (Author)
Keywords	Recoverable booster motors Liquid propellant rocket engines Liquid rocket propellants Liquid rocket oxidizers Liquid rocket fuels Design Performance(Engineering) Lr-129 engines Xlr-129-p-1 engines Cooling Transpiration Underexpanded nozzle flow
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	81G - Rocket Engines & Motors 81H - Rocket Propellants
Corporate Authors	Pratt and Whitney Aircraft, West Palm Beach, FL. Florida Research and Development Center.
Document Type	Technical Report
Title Note	Special rept.
NTIS Issue Number	198615
Contract Number	F04611-68-C-0002