EFFECT OF FINITE THRUSTING TIME IN ORBITAL MANEUVERS

Abstract

1 Melbourne, W. G., Three-dimensional optimum thrust trajectories for power-limited propulsion systems, ARS J. 31, 1723-1728 (1961). 2 Breakwell, J. V., Gillespie, R. W., and Ross, S., Researches in interplanetary transfer, ARS J. 31, 201-208 (1961). 3 Clarke, V. C., Bollman, W. E., and Scholey, W. J., Design parameters for ballistic interplanetary trajectories, Part I: One-way transfer to Mars and Venus, Jet Propulsion Lab., Pasadena, Calif., TR 32-77 (March 1,1962). 4 Bliss, G. A., Lectures on the Calculus Variations (University of Chicago Press, Chicago, 1946), Chaps. 1 and 7. 5 Melbourne, W. G. and Sauer, C. G., Jr., Optimum thrust programs for power-limited propulsion systems, Jet Propulsion Lab., Pasadena, Calif., TR 32-118 (1961); also Astronaut. Acta (to be published). 6 Irving, J. H., Space Technology, edited by H. S. Seifert (John Wiley and Sons Inc., New York, 1959), Chap. 10. 7 Leitmann, G., Minimum transfer time for a power-limited rocket,'' J. Appl. Mech. 28,171-178 (1961). 8 Melbourne, W. G. and Sauer, C. G., Jr., Optimum interplanetary rendezvous trajectories for power-limited vehicles, Jet Propulsion Lab., Pasadena, Calif., TR 32-226 (1962). 9 Melbourne, W. G., Richardson, D. E., and Sauer, C. G., Interplanetary trajectory optimization with power-limited vehicles,, Jet Propulsion Lab., Pasadena, Calif., TR 32-173 (1961). 10 Melbourne, W. G., Interplanetary trajectories and payload capabilities of advanced propulsion vehicles, Jet Propulsion Lab., Pasadena, Calif., TR 32-68 (1961).