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Part image
Hybrid engine by
C7 Aerospace Division and Rockmax Conglomerate
Radial size Small
Cost (total) 5 900.00 Fund
Mass (total) 1.75 t
Drag 0.2
Max. Temp. 3600 K
Impact Tolerance 20 m/s
Research Unknown
Unlock cost {{{unlock cost}}} Fund
Since version 0.23
Part configuration rapierEngine
Liquid fuel engine
Maximum thrust (1 atm) 155.56 kN
(vacuum) 175.00 kN
Isp (1 atm) 320 s
(vacuum) 360 s
Fuel con­sumption (1 atm) 11.15 l/s
(vacuum) 9.91 l/s
Thrust vectoring 3 °
Jet engine
Maximum thrust 190 kN
Stall Threshold  ? kN
Isp 800 s
Fuel con­sumption 0.30 l/s
Intake air consumption 4.54 l/s
Thrust vectoring 3 °

This is an example how I "envision" the next generation of part templates. Current problems with this system:

  • Most of the names are already used
There might be a workaround: Use the same name for both templates, but if the mass parameter is determined it treats it as the old version?
  • There might be multiple properties with the same name (e.g. maximum thrust)
I added headers here manually, in the final version, those headers should be integrated in the subtemplates. Maybe rearrange them, that research and since are not below the specific ones (or separate them with another header)
  • Also some parameters are superfluous (e.g. vectoring)
This might be only the case here, but maybe future other hybrid engines have different vectoring values?