Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"
From Kerbal Space Program Wiki
m (*use the new jet engine module (LFE needs to be updated so temporary solution with the preview template);) |
(+applied reaction engine module;) |
||
| Line 1: | Line 1: | ||
| − | <noinclude>{{Data template used | + | <noinclude>{{Data template used}}</noinclude> |
| − | + | {{Infobox/Part | |
| − | {{Infobox/Part | + | |file=Rapier Engine_01.png |
| − | |file= | + | |role=Hybrid engine |
| + | |parent=Engine | ||
|manufacturer=C7 Aerospace Division | |manufacturer=C7 Aerospace Division | ||
|manufacturer2=Rockmax Conglomerate | |manufacturer2=Rockmax Conglomerate | ||
| Line 11: | Line 12: | ||
|temp=3600 | |temp=3600 | ||
|tolerance=20 | |tolerance=20 | ||
| + | |research=Hypersonic Flight | ||
| + | |since=0.23 | ||
| + | |part=rapierEngine | ||
| + | |more= | ||
| + | {{Infobox/Line|'''Liquid fuel engine'''|style=text-align:center;text-decoration:underline;}} | ||
| + | {{Infobox/Part/reaction engine | ||
|thrust=175 | |thrust=175 | ||
|isp-atm=320 | |isp-atm=320 | ||
|isp-vac=360 | |isp-vac=360 | ||
|vectoring=3 | |vectoring=3 | ||
| − | |||
| − | |||
}} | }} | ||
| − | + | {{Infobox/Line|'''Jet engine'''|style=text-align:center;text-decoration:underline;}} | |
| − | |||
| − | |||
{{Infobox/Part/JetEngine | {{Infobox/Part/JetEngine | ||
|thrust=190 | |thrust=190 | ||
Revision as of 17:08, 10 February 2014
| CR-7 R.A.P.I.E.R. Engine | ||
 | ||
| Hybrid engine by C7 Aerospace Divisionand Rockmax Conglomerate | ||
| Radial size | Small | |
| Cost | (total) | 5 900.00 
|
| Mass | (total) | 1.750 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 | ||
