HYDRA 70 MK66 Aerodynamics and Roll Analysis

Abstract

This report is intended to complement, summarize, and update previous reports on the aerodynamic characteristics of the 2.75 family of rockets. It presents a more detailed basic aerodynamic characterization of the rocket with the two principal warheads that typify most of the configurations of the Hydra 70 system. The reason for publishing this report at this time is that recent studies have suggested application of the MK66 motor, or a derivative thereof, for future systems, and that a more detailed aerodynamic definition in one source may be useful.

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Document Details

Document Type
Technical Report
Publication Date
Jul 23, 1990
Accession Number
ADA226182

Entities

People

  • C. W. Dahlke
  • George Batiuk

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aerodynamic Stability
  • Control Systems
  • Databases
  • Engineering
  • Fire Control Systems
  • Mach Number
  • Munitions
  • Nozzles
  • Rocket Components
  • Rocket Engines
  • Rockets
  • Security
  • Simulations
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Business Analytics
  • Explosive Engineering.
  • Theoretical Analysis.