Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"
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{{Infobox/Part | {{Infobox/Part | ||
|file=Rapier Engine_01.png | |file=Rapier Engine_01.png | ||
| − | | | + | |type=he |
| − | | | + | |size=1 |
| − | |manufacturer=C7 | + | |manufacturer=C7 |
| − | |manufacturer2= | + | |manufacturer2=RMC |
| − | + | |costs=6000 | |
| − | |costs= | + | |mass=2.0 |
| − | |mass= | ||
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=20 | |tolerance=20 | ||
| − | |research= | + | |research=Aerospace Tech |
| + | |unlock cost=35000 | ||
|since=0.23 | |since=0.23 | ||
| + | |filename=rapierEngine.cfg | ||
|part=rapierEngine | |part=rapierEngine | ||
| − | | | + | |parent=Engine |
| − | |more= | + | |more={{Infobox/Part/jet engine |
| − | {{Infobox/Part/ | + | |thrust=105 |
| + | |isp=3200 | ||
| + | |vectoring=3 | ||
| + | |intake=6 | ||
| + | }} | ||
{{Infobox/Part/reaction engine | {{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=180 |
| − | |isp-atm= | + | |isp-atm=275 |
| − | |isp-vac= | + | |isp-vac=305 |
| − | |vectoring=3 | + | |vectoring=3 |
| + | |fuel=lfox | ||
}} | }} | ||
| − | {{Infobox/Part/ | + | {{Infobox/Part/test subject |
| − | + | |environments=127 | |
| − | + | |event=y | |
| − | | | + | |staging=y |
| − | | | ||
| − | | | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:13, 9 October 2024
| CR-7 R.A.P.I.E.R. Engine | ||
 | ||
| Hybrid engine by C7 Aerospace Divisionand Rockomax Conglomerate | ||
| Radial size | Small | |
| Cost | (total) | 6 000.00 
|
| Mass | (total) | 2.000 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 20 m/s | |
| Research |  Aerospace Tech
| |
| Unlock cost | 35 000
| |
| Since version | 0.23 | |
| Part configuration | rapierEngine.cfg | |
| Maximum thrust | 105.00 kN | |
| Isp | (max) | 3200 s |
| Fuel consumption | 0.67  /s
| |
| Intake air consumption | 4.02  /s
| |
| Thrust vectoring | 3 ° | |
| Maximum thrust | (1 atm) | 162.30 kN |
| (vacuum) | 180.00 kN | |
| Isp | (1 atm) | 275 s |
| (vacuum) | 305 s | |
| Fuel consumption | 12.04 /s
| |
| Thrust vectoring | 3 ° | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
