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The Rocket Equation
Vexhaust = Isp * g [d/dt(MV) = 0]
dV = Vexhaust* log( final mass / initial mass)
Material Isp Limitation
- solid fuel 200-250 mass-starved
- LH2/LOX 350-450 mass-starved
- Nuclear Thermal 825-925 mass-starved
- MHD 2000-5000 energy-starved
- ION 3500-10000 energy-starved
- Matter-Antimatter ~1,000,000 mass-starved
- Photons 30,000,000-¥ both-starved
Notes: