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... ld provide more than 400 tonnes of thrust, and after the dismantling, Orion had a mass of 330 tonnes. Based on the conservation of momentum, the rocket engine had to expel enough high-speed mass to effectively reduce Orion’s high speed.
Orion’s computer precisely controlled the engine via a flight program that Tomcat had written. However, to reduce the errors in the Raptor 10D’s thick nozzles to the level of millimeters was impossible. Their original use case was n ...
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