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Submitted: May 13, 2008
File Size: 59.0 KB
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Resolution: 600×450
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Atmospheric computer model flight testing of R&T Projectiles and Ballistics' Low Earth Orbit Interceptor Mark II.

Future revisions call for further modification of the solid rocket booster, augmentation of vertical stabilizers and rudder control surfaces, augmentation of stabilaters and stabilater control surface roots, further development of flight stability augmentation software, and the possible addition of forward canards to reduce dependence on hydrazine attitude thrusters during atmospheric flight.
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