New answers tagged

1

For the abort tests in early 2020, according to documents filed with the FAA over a year prior, the Dragon flew with 2565 kg of propellant (1590 kg of NTO and 975 kg of MMH), but only about half of that was fired during the abort. Consumption rate for a single SuperDraco is about 31 kg/s (= 71kN thrust / 2300 m/s exhaust velocity), so for the suite of 8 ...


Top 50 recent answers are included