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- W2331509922 abstract "To model the dynamics of a craft like the SpaceShipTwo, which loses almost half its mass in under a minute, knowledge of the variations of the mass, inertia tensor and center of gravity becomes important. Equally important is the knowledge of how the thrust varies during the burn. This paper presents a mathematical model of the RocketMotorTwo which is a hybrid rocket motor powering the SpaceShipTwo. This model has been used not only to obtain an accurate representation of the rocket’s thrust profile but also to obtain a profile of how the mass properties of the propulsion system will vary as the rocket motor burns through its HTPB fuel and Nitrous Oxide oxidizer." @default.
- W2331509922 created "2016-06-24" @default.
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- W2331509922 date "2015-07-02" @default.
- W2331509922 modified "2023-09-23" @default.
- W2331509922 title "Mathematical Modelling of RocketMotorTwo" @default.
- W2331509922 cites W2022267340 @default.
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- W2331509922 doi "https://doi.org/10.2514/6.2015-3684" @default.
- W2331509922 hasPublicationYear "2015" @default.
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