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Jeff Stuart 2/14/2008 Dynamics and Controls Spin Stabilization of Third Stage
AAE 450 Spring 2008 1
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Set-Up and Assumptions
Axisymmetric about Distance between cg and cm negligible Out of atmosphere (no drag) Constant mass flow rate Uniform density No initial spin cm S 3rd Stage 2nd Stage Spin Table AAE 450 Spring 2008 2 Dynamics and Controls
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Future Work Further investigate spin and thrust vector control 3
AAE 450 Spring 2008 3 Dynamics and Controls
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Simplified EOMs Kinematic relations developed by A. Chaney 4
AAE 450 Spring 2008 4 Dynamics and Controls
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Spin rate in terms of time
Solution Derivation – Spin-up before engine ignition Spin rate in terms of time AAE 450 Spring 2008 5 Dynamics and Controls
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Scaled Vanguard Data From C. Strauss 6 Dynamics and Controls
AAE 450 Spring 2008 6 Dynamics and Controls
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References Schmidt, James. “Performance of X 258 Third-Stage Motor on Delta 36 (OT-3)”. NASA Report. July 1967 GPS IIR-12 Media Kit. The Boeing Company. 6/6/2005 AAE 450 Spring 2008 7 Dynamics and Controls
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