This simulates a single-stage concept where the vehicle's structure serves as both fuel tank and the main payload (e.g., a potential space station module). Once in orbit, such a structure could potentially be spun for artificial gravity.
Dry Mass: - t
Fuel Mass: - t
Total Mass: - t
Est. Isp: - s
Est. Burn Time: - s
Altitude: 0.0 km
Velocity (H): 0.00 km/s
Fuel: 100.0 %
Sim Speed: 1.0x