Constant thrust programming for a multistage rocket flown in vacuum with a given initial/final thrust-to-weight ratio in an arbitrary stage |
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| Authors: | S N Maitra |
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| Affiliation: | (1) Department of Mathematics, National Defence Academy, P.O. NDA Khadakwasla, 411023 Pune, India |
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| Abstract: | The burn time and burnout velocity of a multistage rocket flown vertically in vacuum with constant thrust tangential to the
flight path and a prescribed initial/final thrust-to-weight ratio in an arbitrary stage have been determined.
The present paper also deals with optimal staging under given conditions of flight. |
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| Keywords: | Constant thrust programming multistage rocket thrust-to-weight ratio burntime burnout velocity |
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