11d426の例文

例文

1. For the orbital correction engine ( SKD ), they developed the 11D426.
2. While slightly less powerful than the 11D426 with, specific impulse increased to and total burn time increased from 570 seconds to 890.
3. For the new and improved high thrust RCS ( DPO-B ), known as the "'11D428 "', they kept the use of 14 thrusters, but instead of H 2 O 2 monopropellant they used the same cycle and propellant as the 11D426 SKD . They also increase the thrust from the previous to.