Difference between revisions of "RV-105 RCS Thruster Block/Box"
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m (!this engine does use monopropellant;) |
m (*update to 0.24.2;) |
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|mass=0.05 | |mass=0.05 | ||
|drag=0.001 | |drag=0.001 | ||
+ | |temp=3600 | ||
|tolerance=15 | |tolerance=15 | ||
− | + | |research=Advanced Flight Control | |
− | |research= | ||
|since=0.11.0 | |since=0.11.0 | ||
|part=RCS block | |part=RCS block | ||
− | |||
|physics insignificant=y | |physics insignificant=y | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine |
Revision as of 01:22, 12 August 2014
RV-105 RCS Thruster Block | ||
by STEADLER Engineering Corps | ||
Cost | (total) | 450.00 |
Mass | (total) | 0.050 t [1] |
Drag | 0.001 [1] | |
Max. Temp. | 3600 K | |
Impact Tolerance | 15 m/s | |
Research | Advanced Flight Control | |
Unlock cost | 0 | |
Since version | 0.11.0 | |
Part configuration | [[Parts/RCS block/{{{filename}}}|{{{filename}}}]] | |
Maximum thrust | (1 atm) | 0.38 kN |
(vacuum) | 1.00 kN | |
Isp | (1 atm) | 100 s |
(vacuum) | 260 s | |
Fuel consumption | 0.10 /s | |
Thrust vectoring | No | |
Thrust vectors | 4 (sideways) | |
|