Minimum Transfer Time for a Power-Limited RocketSource: Journal of Applied Mechanics:;1961:;volume( 028 ):;issue: 002::page 171Author:George Leitmann
DOI: 10.1115/1.3641648Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The problem considered is that of determining the acceleration program leading to minimum transfer time for a power-limited rocket moving between prescribed positions and velocities in a constant gravitational field. It is found that flight must take place at maximum power and that the thrust-acceleration components are linear functions of time. The case of rectilinear transfer between positions of rest is treated in detail, and the results are compared with those previously obtained for a constant-acceleration transfer.
keyword(s): Rockets , Flight , Thrust AND Functions ,
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contributor author | George Leitmann | |
date accessioned | 2017-05-09T00:37:02Z | |
date available | 2017-05-09T00:37:02Z | |
date copyright | June, 1961 | |
date issued | 1961 | |
identifier issn | 0021-8936 | |
identifier other | JAMCAV-25616#171_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/142834 | |
description abstract | The problem considered is that of determining the acceleration program leading to minimum transfer time for a power-limited rocket moving between prescribed positions and velocities in a constant gravitational field. It is found that flight must take place at maximum power and that the thrust-acceleration components are linear functions of time. The case of rectilinear transfer between positions of rest is treated in detail, and the results are compared with those previously obtained for a constant-acceleration transfer. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Minimum Transfer Time for a Power-Limited Rocket | |
type | Journal Paper | |
journal volume | 28 | |
journal issue | 2 | |
journal title | Journal of Applied Mechanics | |
identifier doi | 10.1115/1.3641648 | |
journal fristpage | 171 | |
journal lastpage | 178 | |
identifier eissn | 1528-9036 | |
keywords | Rockets | |
keywords | Flight | |
keywords | Thrust AND Functions | |
tree | Journal of Applied Mechanics:;1961:;volume( 028 ):;issue: 002 | |
contenttype | Fulltext |