Ablative Laser Propulsion: Specific Impulse and Thrust Derived from Force Measurements
Author:
Affiliation:
1. University of Alabama in Huntsville, Huntsville, Alabama 35899
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1567
Reference13 articles.
1. Ablative Laser Propulsion: An Old Concept Revisited
2. Concepts and status of laser-supported rocket propulsion
3. Laser Ablation
4. Specific Impulse and Other Characteristics of Elementary Propellants for Ablative Laser Propulsion
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