Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"
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Revision as of 00:52, 8 October 2014
CR-7 R.A.P.I.E.R. Engine | ||
Hybrid engine by C7 Aerospace Divisionand Rockomax Conglomerate | ||
Radial size | Small | |
Cost | (total) | 3 600.00 |
Mass | (total) | 1.200 t |
Drag | 0.2 | |
Max. Temp. | 3600 K | |
Impact Tolerance | 20 m/s | |
Research | Hypersonic Flight | |
Unlock cost | 0 | |
Since version | 0.23 | |
Part configuration | [[Parts/Engine/rapierEngine/{{{filename}}}|{{{filename}}}]] | |
Liquid fuel engine | ||
Maximum thrust | (1 atm) | 155.56 kN |
(vacuum) | 175.00 kN | |
Isp | (1 atm) | 320 s |
(vacuum) | 360 s | |
Fuel consumption | 9.91 /s | |
Thrust vectoring | 3 ° | |
Jet engine | ||
Maximum thrust | 190.00 kN | |
Isp | (max) | 800 s |
Fuel consumption | 4.84 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | 3 ° |