REFERENCES
- DAVID BUDEN, “Operational Characteristics of Nuclear Rockets,” J. Spacecraft Rockets, 7, 832 (1970).
- J. H. ALTSEIMER, G. F. MADER, and J. J. STEWART, “Operating Characteristics and Requirements for the NERVA Flight Engine,” Paper No. 70-676 presented at the AIAA 6th Propulsion Joint Specialist Conference, San Diego, California (1970).
- Modular Nuclear Vehicle Design, Asymmetric Propellant Heating Computer Program, Report No. A794909A, Lockheed Missile and Space Company (September 1968).
- R. J. STOCHL et al., “Gaseous Hydrogen Pressurant Requirements for Discharge of Liquid Hydrogen from a 3.96 Meter (13 ft) Diameter Spherical Tank,” NASA-TND-5387, Lewis Research Center (August 1969).
- Proc. Conf. Propellant Tank Pressurizatìon and Stratification, Vol. 2, National Aeronautics and Space Administration (January 1965).
- Propellant Tank Pressurization and Heating Computer, Program-D-35206, NERVA Rocket Operations, Aerojet Nuclear Systems Company (1970), to be published.