HIGH OPERATIONS TEMPO ENERGETIC ACCESS TO GLOBE AND LAUNCH EXPERIMENT (HOT EAGLE). Phase 1

Abstract

In this report, the researchers defined and assessed a reusable launch vehicle upper stage that is suitable for use with areusable first stage. A subscale demonstrator that is intended for the flight test validation of key HOT EAGLEtechnologies and system concepts has been defined and sized to allow flight on an existing first-stage booster. This reportalso includes studies on propulsion, structure, and systems and avionics.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2006
Accession Number
AD1005980

Entities

People

  • Daniel P. Raymer

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • C4I
  • Counter WMD
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Configurations
  • Aircrafts
  • Airframes
  • Composite Materials
  • Computational Fluid Dynamics
  • Control Systems
  • Failure Mode And Effect Analysis
  • Horizontal Stabilizers
  • Inertial Navigation
  • Inertial Navigation Systems
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Navigation

Fields of Study

  • Physics

Readers

  • Organizational Process Management (OPM).
  • Rocket Propulsion.
  • Software Engineering