CE-20 is a cryogenic rocket engine being developed by the Liquid Propulsion Systems Center a subsidy of ISRO. It is developed to power the upper stage of GSLV-Mk.3 .It is a first Indian cryogenic engine to feature a gas generator cycle . It burns a mixture of liquid hydrogen and liquid oxygen and generates a thrust of 200kn. Its thrust can set between 180 kn to 220 kn .
- Operating Cycle - Gas Generator
- Propellant Combination - Liquid oxygen / Liquid hydrogen
- Thrust Nominal (Vacuum) - 200 kN
- Operating Thrust Range - 180 kN to 220 kN (To be set at any fix values)
- Chamber Pressure (Nom) - 6 MPa
- Engine Mixture ratio (Oxidizer/Fuel by weight) - 5.05
- Engine Specific Impulse - 443 ± 3 seconds (4.344 ± 0.029 km/s)
- Engine Burn Duration (Nom) - 595 seconds
- Total Flow rate - 462 kg/s
- Nozzle Area ratio - 100
- Mass - 588 kg
888 Casino App Download for Android (.apk) & iPhone
ReplyDelete888 Casino Mobile App. We have a huge list 김해 출장마사지 of mobile 나주 출장안마 slots, 수원 출장안마 including progressive jackpots, live dealer 제천 출장마사지 games, and slots that you can 수원 출장샵 play at
Understanding BDG Win Account Sign Up starts with reviewing the registration instructions and account requirements. Users should keep passwords confidential, read the privacy policy, and make sure they meet all relevant eligibility conditions before proceeding.
ReplyDelete