Space Propulsion - IAP/TU Wien
Space Propulsion - IAP/TU Wien
Space Propulsion - IAP/TU Wien
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<strong>Space</strong> <strong>Propulsion</strong><br />
finite burn losses<br />
thrust vector is held inertially fixed during the burn<br />
orbital elements change continuously during burn<br />
angle between thrust and velocity increases during burn<br />
at constant thrust, acceleration in flight direction decreases during burn