Share Email Print

Proceedings Paper

Laser-based particle protection system for spacecraft in low-earth orbit
Author(s): David L. Snodgrass II; Roger A. Dougal
Format Member Price Non-Member Price
PDF $17.00 $21.00

Paper Abstract

A particle deflector operating on the principle of laser-induced ablation may eliminate collisions between spacecraft and small debris in low earth orbit. A practical system is constrained to deflecting particles up to a few grams mass with velocities up to 10 km/s. Fundamental concerns for such a system include particle detection and tracking, beam formation, beam steering, and energy coupling to the target. The limiting technology is the detection and tracking system, which must located fast moving (10 km/s) objects 1 cm or smaller in diameter at distances greater than 1 km. We show that a 2000 J laser beam can deflect at 10 mrad a 1-g particle approaching at 10 km/s--adequate to protect a modest sized (approximately 10 m) space structure if the particle is intercepted while still 1 km away. Methods for delivering large optical power densities onto a small (approximately 1 cm) target over moderate (1000 m) distances are proposed.

Paper Details

Date Published: 8 June 1994
PDF: 10 pages
Proc. SPIE 2214, Space Instrumentation and Dual-Use Technologies, (8 June 1994); doi: 10.1117/12.177661
Show Author Affiliations
David L. Snodgrass II, Univ. of South Carolina (United States)
Roger A. Dougal, Univ. of South Carolina (United States)

Published in SPIE Proceedings Vol. 2214:
Space Instrumentation and Dual-Use Technologies
Firooz A. Allahdadi; Michael Chrisp; Concetto R. Giuliano; W. Pete Latham; James F. Shanley, Editor(s)

© SPIE. Terms of Use
Back to Top