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Interesting side note regarding dad's involvement in the minuteman projects:
in the early 60's he was chosen as part of the team to develop the advanced minutemen design and proposal (MMII). In that process he came up with a way to use an unconventional design of shape charges for thrust termination, which was 400 pounds lighter than the existing design on the MM. He was given the green light for development and it proved successful, and his design was adopted by the air force on the MMII and also the Poseidon (C-4) and Trident (D-5) upper stages for the navy. At that time the Air Force stated that the reduction of weight of upper stages was worth $1 million per pound. |
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Found this re: dad's thrust termination design ....
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And they did it with slide rules.
http://forums.pelicanparts.com/uploa...1386184600.jpg http://forums.pelicanparts.com/uploa...1386184612.jpg When the computer senses the missile has reached the correct point in its flight path, thrust termination (TT) ports in the front of the third-stage motor are opened for negative thrust. The post-boost vehicle (PBV) separates from the third stage motor and is maneuvered by the MGS to the pre-determined points of RV deployment. The RVs are then pre-armed and separated one at a time from the post-boost system. The RVs follow individual ballistic trajectories, reenter the earth's atmosphere, arm, and detonate according to the planned target profile. |
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