The special-purpose engine thrust difference influence on the control object motion characteristics
Authors: Ivanov A.V., Kirakosyants A.T.
Published in issue: #7(151)/2024
DOI: 10.18698/2308-6033-2024-7-2372
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts
The paper substantiates necessity to ensure single-thrust performance of the special-purpose engines as part of a space rocket, namely the head end spinning engines and the rocket nose cone retraction engines. It provides description of the conditions these engines are operating. Various possible cases of the head end motion are considered, when it is exposed to external forces, using the modern SolidWorks computer-aided design system package, which makes it possible to confirm possibility of using this package in simulating and predicting the control object behaviour taking into account the special-purpose engine thrust difference. The research conducted provides recommendations in designing special-purpose engines, as well as in positioning these engines as a spacecraft component to ensure successful completion of its assigned flight task.
EDN RWROPE
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