Difference between revisions of "CR-7 R.A.P.I.E.R. Engine/Box"

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m (*update to 0.24.2;)
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{{Infobox/Part/jet engine
 
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Revision as of 00:52, 8 October 2014

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
CR-7 R.A.P.I.E.R. Engine
Part image
Hybrid engine by
C7 Aerospace Divisionand Rockomax Conglomerate

Radial size Small
Cost (total) 3 600.00 Funds
Mass (total) 1.20 t
Drag 0.2
Max. Temp. 3600 K
Volume  ?
Impact Tolerance 20 m/s
Research Hypersonic flight.png Hypersonic Flight
Unlock cost 0 Funds
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 Units of fuel/s


Thrust vectoring 3 °
Jet engine
Maximum thrust 190 kN
Isp (max) 800 s
Fuel consumption 4.84 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring 3 °