THE OPTIMUM OPERATION OF ENERGYRESTRICTED ROCKETS, INCLUDING RELATIVISTIC EFFECTS,
Abstract
If the total energy available for the propulsion of a rocket is restriced while the exhaust velocity may be varied, it has been shown that the rocket performance can be improved by certain 'tayloring' of the exhaust speed. This concept is discussed in terms of relativistic mechanics.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1960
- Accession Number
- AD0621387
Entities
People
- J. Ackeret
- Nicholas Rott
Organizations
- University of California, Los Angeles