Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"
From Kerbal Space Program Wiki
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.) |
m (*update to 1.0;) |
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|manufacturer=C7 | |manufacturer=C7 | ||
|manufacturer2=RMC | |manufacturer2=RMC | ||
− | |costs= | + | |costs=6000 |
− | |mass= | + | |mass=2.0 |
|drag=0.2 | |drag=0.2 | ||
− | |temp= | + | |temp=2000 |
|tolerance=20 | |tolerance=20 | ||
− | |research= | + | |research=Aerospace Tech |
|unlock cost=35000 | |unlock cost=35000 | ||
|since=0.23 | |since=0.23 | ||
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{{Infobox/Part/title|lfe}} | {{Infobox/Part/title|lfe}} | ||
{{Infobox/Part/reaction engine | {{Infobox/Part/reaction engine | ||
− | |thrust= | + | |thrust=162.3 |
− | |isp-atm= | + | |isp-atm=275 |
− | |isp-vac= | + | |isp-vac=305 |
|vectoring=3 | |vectoring=3 | ||
|fuel=lfox | |fuel=lfox | ||
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{{Infobox/Part/title|je}} | {{Infobox/Part/title|je}} | ||
{{Infobox/Part/jet engine | {{Infobox/Part/jet engine | ||
− | |thrust= | + | |thrust=140 |
|vectoring=3 | |vectoring=3 | ||
− | |isp= | + | |isp=6400 |
}} | }} | ||
}} | }} |
Revision as of 17:03, 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) | 6 000.00 |
Mass | (total) | 2.00 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 | |
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) | 146.34 kN |
(vacuum) | 162.30 kN | |
Isp | (1 atm) | 275 s |
(vacuum) | 305 s | |
Fuel consumption | 10.85 /s | |
Thrust vectoring | 3 ° | |
Jet engine | ||
Maximum thrust | 140.00 kN | |
Isp | (max) | 6400 s |
Fuel consumption | 0.45 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | 3 ° |