Absorption of thermal radiation in the transparent wall of a nuclearlight bulb rocket engine.
Author:
Affiliation:
1. United Aircraft Research Laboratories, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28948
Reference5 articles.
1. March 1965;Douglas F. C.,1965
2. Opacity of High-Temperature Air
3. ABSORPTION COEFFICIENTS OF HEATED AIR: A COMPILATION TO 24,000 K. VOLUME 1
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1. A Proposal for Using Nuclear Reactors as Thermal Radiation Sources;Nuclear Technology;1971-01
2. Gas-core nuclear rocket engine technology status;Journal of Spacecraft and Rockets;1970-12
3. Gas core nuclear rocket engine technology status;6th Propulsion Joint Specialist Conference;1970-06-15
4. Survey of advanced concepts in nuclear propulsion.;Journal of Spacecraft and Rockets;1968-10
5. Open-cycle and light-bulb types of vortex- stabilized gaseous nuclear rockets.;Journal of Spacecraft and Rockets;1968-08
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