Difference between revisions of "Template:Infobox/Part/reaction engine"
From Kerbal Space Program Wiki
< Template:Infobox | Part
m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';) |
m (*renamed Parameter Table to Parameter table;) |
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* [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}} | * [[Jet engine]]s: {{Tl|Infobox/Part/jet engine}} | ||
− | {{Parameter | + | {{Parameter table|name=text|parameters= |
{{Parameter row|thrust|Maximum thrust in kN}} | {{Parameter row|thrust|Maximum thrust in kN}} | ||
{{Parameter row|isp-atm|Specific impulse at Kerbin's sea level (1 atm)}} | {{Parameter row|isp-atm|Specific impulse at Kerbin's sea level (1 atm)}} |
Revision as of 12:07, 19 December 2014
Maximum thrust | 175 kN | |
Isp | (1 atm) | 388 s |
(vacuum) | 390 s | |
Thrust vectoring | No |
{{Infobox/Part}} modules for reaction engines. Use this module directly for liquid fuel engines and RCS thrusters. It uses {{Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust. Other engine types:
- Solid rocket boosters: {{Infobox/Part/solid fuel engine}} (uses this template)
- Ion engines: {{Infobox/Part/ion engine}} (uses this template)
- Jet engines: {{Infobox/Part/jet engine}}
Name | Optional | Description | Default |
---|---|---|---|
thrust | No | Maximum thrust in kN | |
isp-atm | No | Specific impulse at Kerbin's sea level (1 atm) | |
isp-vac | Yes | Specific impulse in vacuum. | Atmospheric Isp |
vectoring | Yes | Thrust vectoring, if not set displays “No”. | Not set/No |
fuel | Yes | Type of fuel. Supported:
|
lfox |