Abstract

References 1 Burch, B. A., of Contamination on Spacecraft Surfaces Exposed to Rocket Exhausts/' AEDC-TR-68-23, April 1968. ARO Inc., Tullahoma, Tenn. 2 Hill, D. W., Jr. and Smith, D. K., and Control of Contamination from a Scaled MOL Altitude Control Thruster in a Tangential Orientation/' AEDC-TR-69-146, Oct. 1969, ARO Inc., Tullahoma, Tenn. 3 Borson, E. N. and Landsbaum, E. M., A Review of Available Rocket Contamination Results, TR-0200(4250-20)-2, Dec. 1969. Aerospace Corp., El Segundo, Calif. 4 Valentine, R. S., Rossi, F. S., and Kromfrey, R. K., Fluid Dynamic Effects on Apollo Engine Pressure Spikes, Journal of Spacecraft and Rockets, Vol. 5, No. 1, Jan. 1968, pp. 31-35. 5 Christos, T. et al., Characteristics of Condensed-Phase Hydrazine-Type Fuels with Nitrogen Tetroxide/' Journal of Spacecraft and Rockets, Vol. 4, No. 9, Sept. 1967, pp. 1224-1229. 6 Per lee, H. E. et al., Preignition Phenomena in Small A-50/NTO Pulsed Rocket Engines, Journal of Spacecraft and Rockets, Vol. 5, No. 2, Feb. 1968, pp. 233-235. 7 Mayer, S. W., Taylor, D., and Schieler, L., Preignition Products from Propellants at Simulated High-Altitude Conditions, Combustion Science and Technology, Vol. 1, 1969, pp. 119-129. 8 Seamans, T. F. and Dawson, B. E., Hyperbolic Ignition at Reduced Pressures, Rept. RMD 5809-Q1, 1966, Thiokol Chemical Corp. 9 Takimoto, H. H. and Denault, G. C., Residues from N2O4-MMH Motors, TR-0066(5210-10)-1, Sept. 1969, Aerospace Corp., El Segundo, Calif.

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