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NASA NTRS · 20040170454

Specific Impulse Definition for Ablative Laser Propulsion

Abstract

The term "specific impulse" is so ingrained in the field of rocket propulsion that it is unlikely that any fundamental argument would be taken seriously for its removal. It is not an ideal measure but it does give an indication of the amount of mass flow (mass loss/time), as in fuel rate, required to produce a measured thrust over some time period This investigation explores the implications of being able to accurately measure the ablation rate and how the language used to describe the specific impulse results may have to change slightly, and recasts the specific impulse as something that is not a time average. It is not currently possible to measure the ablation rate accurately in real time so it is generally just assumed that a constant amount of material will be removed for each laser pulse delivered The specific impulse dependence on the ablation rate is determined here as a correction to the classical textbook definition.

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BibTeXRIS

Herren, Kenneth A., Gregory, Don A.. 2004-01-01. Specific Impulse Definition for Ablative Laser Propulsion. https://ntrs.nasa.gov/citations/20040170454

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