Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"
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m (BobBot moved page R.A.P.I.E.R. Engine/Box to CR-7 R.A.P.I.E.R. Engine/Box: Renamed part after update.) |
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Revision as of 17:02, 29 April 2015
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 | 35 000 | |
Since version | 0.23 | |
Part configuration | rapierEngine.cfg | |
Testing Environments | ||
On the surface | Yes | |
In the ocean | Yes | |
On the launchpad | Yes | |
In the atmosphere | Yes | |
Sub-orbital | No | |
In an orbit | No | |
On an escape | No | |
Docked | No | |
Test by staging | Yes | |
Manually testable | Yes | |
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) | 2500 s |
Fuel consumption | 1.55 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | 3 ° |