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?
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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