An orbital transfer vehicle between the Lunar Gateway and Low Lunar Orbit has a specific impulse of 300 sec, a MEV dry mass of 2400 kg, and a MPV for the propellant mass of 1100 kg. What is the propellant margin for a mission requiring a 30 AV of 900 m/s?
An orbital transfer vehicle between the Lunar Gateway and Low Lunar Orbit has a specific impulse of 300 sec, a MEV dry mass of 2400 kg, and a MPV for the propellant mass of 1100 kg. What is the propellant margin for a mission requiring a 30 AV of 900 m/s?
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![An orbital transfer vehicle between the Lunar Gateway and Low Lunar Orbit has a
specific impulse of 300 sec, a MEV dry mass of 2400 kg, and a MPV for the propellant mass
of 1100 kg. What is the propellant margin for a mission requiring a 30 AV of 900 m/s?](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F6763f5b2-c545-4efd-97fd-9a12a2a3ca9f%2Ff69ab1fb-99dd-4263-ba7b-27ad6d4f47d4%2Frg8opaw_processed.jpeg&w=3840&q=75)
Transcribed Image Text:An orbital transfer vehicle between the Lunar Gateway and Low Lunar Orbit has a
specific impulse of 300 sec, a MEV dry mass of 2400 kg, and a MPV for the propellant mass
of 1100 kg. What is the propellant margin for a mission requiring a 30 AV of 900 m/s?
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