Elements of Spacecraft Design

References

  1. Ring, E., Rocket Propellant and Pressurization Systems, Prentice Hall, Upper Saddle River, NJ, 1964.

  2. Sutton, G. P., Rocket Propulsion Elements, Wiley, New York, 1986.

  3. Koelle, H. H. (ed.), Handbook of Astronautical Engineering, McGraw Hill, New York, 1961.

  4. Seifert, H. S. (ed.), Space Technology, Wiley, New York, 1959.

  5. Brown, C. D., Spacecraft Mission Design, 2nd ed. AIAA, Reston, VA, 1998.

  6. Brown, C. D., Spacecraft Propulsion, AIAA, Reston, VA, 1996.

  7. Monopropellant Hydrazine Design Data, Rocket Research Corp. Seattle, WA.

  8. Morningstar, R. E., Kaloust, A. H., and Macklis, H., "An Operational Satellite Propulsion System Providing for Vernier Velocity, High and Low Level Attitude Control and Spin Trim," AIAA, Paper 72-1130, 1972.

  9. Sackheim, R. L., "Survey of Space Applications of Monopropellant Hydrazine Propulsion Systems," AIAA Paper 74-42367, 1974.

  10. Hearn, H. C., "Design and Development of a Large Bipropellant Blowdown Propulsion System," AIAA Paper 93-2118, 1993.

  11. Schmitz, B. W., Groudle, T. A., and Kelley, J. H., "Development of the Post Injection System for Mariner C Spacecraft," Jet Propulsion Lab. Technical Rept. 32-830, California Inst. of Technology, Pasadena, CA, 1966.

  12. "LANDSAT 3 Reference Manual," General Electric Space Div. Philadelphia, PA, 1978.

  13. Holmberg, N. A., Faust, R. P., and Holt, H. M., "Viking '75 Spacecraft Design and Test Summary," NASA RP 1027, 1980.

  14. Frazier, R. E., "HEAO Case Study in Spacecraft Design," TRW Defense and Space Systems Group, Rept. 26000-100-102, AIAA Case Study, July 1981.

  15. Schatz, W. J., Cannova, R. D., Cowley, R. T., and...

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