You're designing a mission with a special type of rocket, a nuclear thermal rocket (NTR). Since it uses a nuclear reactor to heat the propellant, it can achieve an exhaust velocity of Vex = 5.65 km/s. The crew's habitat space, the rocket itself, the shadow shield to protect from radiation, and the instrument payload for scientific research all have a combined mass of 607 x 103 kg, and the propellant is 3,638 x 103 kg. What is the total delta-V of the rocket in km/s?
You're designing a mission with a special type of rocket, a nuclear thermal rocket (NTR). Since it uses a nuclear reactor to heat the propellant, it can achieve an exhaust velocity of Vex = 5.65 km/s. The crew's habitat space, the rocket itself, the shadow shield to protect from radiation, and the instrument payload for scientific research all have a combined mass of 607 x 103 kg, and the propellant is 3,638 x 103 kg. What is the total delta-V of the rocket in km/s?
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Transcribed Image Text:You're designing a mission with a special type of
rocket, a nuclear thermal rocket (NTR). Since it
uses a nuclear reactor to heat the propellant, it
can achieve an exhaust velocity of vex = 5.65
km/s. The crew's habitat space, the rocket
itself, the shadow shield to protect from
radiation, and the instrument payload for
scientific research all have a combined mass of
607 x 103 kg, and the propellant is 3,638 x
103 kg. What is the total delta-V of the rocket
in km/s?
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