Difference between revisions of "O-10 "Puff" MonoPropellant Fuel Engine/Box"

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m (+image;)
(*Release mass is larger. Sort of.)
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Revision as of 19:25, 18 July 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).
O-10 "Puff" MonoPropellant Fuel Engine
Part image
Liquid fuel engine by
Reaction Systems Ltd
Radial size Radial mounted
Cost (total) 800.00 Funds
Mass (total) 0.00 t
Drag 0.2
Max. Temp. 3600 K
Impact Tolerance 7 m/s
Research Unknown
Unlock cost 0 Funds
Since version 0.24
Part configuration Unknown cfg
Maximum thrust (1 atm) 15.17 kN
(vacuum) 20.00 kN
Isp (1 atm) 220 s
(vacuum) 290 s
Fuel consumption 1.76 Units of fuel/s

Thrust vectoring × No