1. Flow Metering Venturis for S-II and S-IV Four-Engine Models;Hendershot,1964
2. Farmer, R., personal communication, NASA Marshall Space Flight Center, 1967.
3. “Theoretical Performance of Liquid Oxygen and RP-1 and Gaseous Oxygen and Gaseous Ethylene as Rocket Propellants,” The Boeing Co., (author and date unknown).
4. Base Heating Progress Rept. 1, Contract NAS 8–20027, Feb. 1965, Cornell Aeronautical Lab.
5. Klein, L. and Penzias, G.J., “Spectral Radiance Measurements of Model Rocket Exhaust Gases at Simulated Altitude, Using a Rapid Scanning Spectrometer,” Paper 67–10, Jan. 1967, AIAA; also AIAA Journal, Vol. 5, No. 9, Sept. 1967, pp. 1690 and 1692.