30 Jun 2022, 14:13
To recap:
1.) A nuclear thermal rocket has roughly twice the ISP of a chemical-based one, and is usually proposed to "burn" hydrogen due to its extremely low molecular weight
2.) A nuclear pulse engine (NPP) produces thrust by exploding nuclear-fissile and/ or fusionable materials, where, the radiation from the blast radiates in all directions, including back towards the ship, providing an impulse to the vehicle
3.) Typically, you have high thrust and low thrust duration, or low thrust and high thrust duration. An antimatter rocket promises, in theory, both worlds: high thrust like a chemical rocket and high thrust duration like an ion engine. In theory, an antimatter rocket could reach high fractional C (speed of light in a vacuum)
4.) Nearly all proposed nuclear "propulsion" concepts proposed thus far are reaction-based; some exotic concepts exist which will be explored at a later time
I will explore nuclear power in space (and on planetary bodies) in the next cycle of Space Nuclear Propulsion/ Power
Theme: Space Nuclear Propulsion/ Power
Have F110, Block 70, will travel