Design Rules and Issues with Respect to Rocket Based Combined Cycles

Abstract

JAXA Kakuda space center has been studying rocket based combined cycle engine for the future space transportation system. This note summarized design process and points that required for detail investigation. Moreover, this note presents our design example of the engine and experimental results with a sub-scale engine tests from the sea-level to the hypersonic conditions.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2010
Accession Number
ADA596260

Entities

People

  • Tetsuo Hiraiwa

Organizations

  • Japan Aerospace Exploration Agency

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Breathing
  • Air Breathing Engines
  • Combustion
  • Combustors
  • Ignition
  • Jet Engines
  • Mach Number
  • Pressure Distribution
  • Ramjet Engines
  • Respiration
  • Rocket Engines
  • Rockets
  • Sea Level
  • Space Transportation
  • Supersonic Combustion Ramjet Engines
  • Test Facilities
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering.
  • Rocket Propulsion.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Space