The objective of this program is to assess the feasibility of the beamed energy propulsion concept for Air Force missions. The work is divided into three major tasks: (1) system studies; (2) theoretical analyses of the coupling mechanisms between the beamed energy and propellant working fluid and (3) preparation of a test plan for the experimental investigation of the coupling processes for various laser/propellant combinations. The results of the study indicate that beamed energy propulsion is technically feasible. No fundamental obstacles have been identified. However considerable technical development is needed in many areas before the concept can be operationally implemented. Three promising applications have been identified. The laser powered tug can be cost effective compared to an advanced cryogenic tug. Apsidal rotation correction and drag make-up are two other missions where significant advantages may be realized for the laser powered concept. Extensive hardware development is required. Critical areas include the lasers, thrusters, thruster reaction chamber windows and the collection and coupling subsystems.
Investigation of Beamed Energy Concepts for Propulsion. Laser/Propellant Coupling Analyses. Volume II
1976
132 pages
Report
No indication
English
Unmanned Spacecraft , Combustion, Engines, & Propellants , Laser beams , Liquid rocket propellants , Space propulsion , Thrusters , Coupling(Interaction) , Hydrogen , Ammonia , Lithium , Decomposition , Carbon monoxide , Absorption coefficients , Inverse scattering , Bremsstrahlung , Computer programs , Mathematical analysis , Molecular vibration , Delaval nozzles , Laser propulsion , Methanol
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