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

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.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1969
Accession Number
AD0500578

Entities

People

  • Robert R. Atherton

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Axial Flow
  • Bell Nozzles
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Contracts
  • Engineering
  • Exhaust Nozzles
  • Flow
  • High Altitude
  • High Pressure
  • Low Altitude
  • Materials
  • Propulsion Systems
  • Rocket Engines
  • Sea Level

Fields of Study

  • Physics

Readers

  • Life Cycle Cost Analysis
  • Rocket Propulsion.
  • Software Engineering