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Project Daedalus
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==Specifications== *Overall length: 190 metres *Payload mass: 450 tonnes {| class="wikitable" ! Property ! First stage !! Second stage |- | Empty mass | 1,690 tonnes (at staging) || 980 tonnes (at cruise speed) |- | Propellant mass | 46,000 tonnes || 4,000 tonnes |- | Engine burn time | 2.05 years || 1.76 years |- | Thrust | 7,540,000 [[newton (unit)|newton]]s || 663,000 newtons |- | Engine exhaust velocity | 10,600,000 m/s || 9,210,000 m/s |- |[[Delta-V]] |35,000,000 m/s (0.117c) |13,000,000 m/s (0.0432c) |}
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