Examples of Technology Transfer from the SDIO Kinetic Energy Weapon Lethality Program to Orbital Debris Modeling

Abstract

The Defense Nuclear Agency (DNA) Kinetic Energy Weapon Lethality and Target Hardening Program (LTH-5) has studied hypervelocity impacts on simple and complex targets for a number of years on behalf of the Strategic Defense Initiative Organization (SDIO). The test parameter space includes projectile masses from 0.1 - 93 grams and velocities ranging from 1 .9 km/s. The work to date includes experimentation and modeling and the resulting data and codes can be made available to the Orbital Debris Spacecraft Breakup Modeling Program through technology transfer. This will reduce duplication, conserve scarce R&D funds, and provide a head start to orbital debris breakup modeling efforts. This paper highlights results from those LTH-5 activities which will be of most interest to those involved with orbital debris generation and the effects of debris on spacecraft. The attached bibliography documents some LTH-5 efforts which are directly applicable to orbital debris breakup modeling.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1991
Accession Number
ADA344572

Entities

People

  • Dennis L. Jones
  • John C. Connell Jr.
  • William J. Tedeschi

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Ballistic Missiles
  • Department Of Defense
  • Explosive Charges
  • Explosives
  • High Explosives
  • Hypervelocity Impact
  • Kill Vehicles
  • Kinetic Energy
  • Materials
  • Propellants
  • Space Debris
  • Space Systems
  • Spacecraft
  • Submarine Launched Ballistic Missiles
  • Technology Transfer
  • Weapon Lethality

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Defense Technology Research and Development.
  • ballistics.

Technology Areas

  • Hypersonics
  • Space
  • Space - Orbital Debris