HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 13. PRELIMINARY MODEL SPECIFICATION FOR CONTINENTAL MODEL 357-1 ENGINE

Abstract

The report contains Continental Preliminary Model Specification No. 2253-A, which contains requirement, capability, and engine performance data on the Continental Model 357-1 (1700-pound thrust) turbojet engine for helicopter rotor-tip mounting.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625823

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Airframes
  • Calorific Value
  • Classification
  • Engines
  • Helicopter Rotors
  • Helicopters
  • Ignition
  • Ignition Systems
  • Jet Aircraft
  • Jet Engines
  • Sea Level
  • Specifications
  • Standards
  • Turbines
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering