MODEL SPECIFICATION LIQUID PROPELLANT ROCKET ENGINE ROCKETDYNE MODEL YLR101-NA-15 (VERNIER)

Abstract

Specification requirements for the YLR101-NA-15 rocket engine are reported. The engine is a calibrated, fixed-thrust bipropellant rocket engine with a nominal sea-level tank-fed rating of 525 pounds. The single thrust chamber shall be gimbal mounted, shall have an exhaust-nozzle expansion ratio of 5.6:1, and shall be regenera tively cooled using the fuel as the heat transfer medium.

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Document Details

Document Type
Technical Report
Publication Date
May 31, 1963
Accession Number
AD0409534

Entities

People

  • B. H. Mccurdy

Tags

DTIC Thesaurus Topics

  • Altitude Chambers
  • Checkout Procedures
  • Engine Components
  • Engines
  • Ignition
  • Ignition Systems
  • Liquid Propellant Rocket Engines
  • Liquid Propellants
  • Materials Processing
  • Rocket Engines
  • Space Systems
  • Test And Evaluation
  • Test Equipment
  • Test Facilities
  • Test Methods
  • Time Intervals
  • Word Processors

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Rocket Propulsion.