The concept, as I worked on it-
So, anybody want to help me out with this concept?
- About big enough to fit on a Jupiter 246 or Ares V. So, no wider than about 8m, no heavier (fully loaded) than 160,000 lbs.
- Nuclear engine. Perhaps two versions to test out a nuclear thermal rocket or VASMIR-type setup. Both will be powered by a nuclear reactor (bimodal for the nuclear thermal rocket). "Shadow shield" drive plate between the engines and the rest of the ship.
- Fuel is liquid hydrogen, with the option of liquid oxygen. Fuel tanks are designed to be removed, for refueling and/or using the tanks for volatile storage (i.e. dropping a few on the moon, pumping in liquid oxygen from lunar oxygen production).
- Significant RCS array. Probably just a "vent" thruster system using the main fuel (easier than trying to figure out how to handle fuel and such-an option would be to use a small, integral liquid oxygen tank to the liquid hydrogen tanks for more "proper" thruster).
- Cargo clamps on the front, "side mount" clamps on the side. I could easily see a Mars mission being built of about five Ishtar boosters, using four to get to Mars with a full load of cargo (crew modules, landers, etc), and using the single remaining engine for the return trip.
So, anybody want to help me out with this concept?