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Template:Infobox part/doc: Difference between revisions

Template page
(just account for all the relevant resources directly, avoid modulization)
Tag: 2017 source edit
(implementing new subbox approach for part module info)
Tag: 2017 source edit
Line 4: Line 4:
| image    = [[File:LV-SW_SWERV.png|200px|center]]  
| image    = [[File:LV-SW_SWERV.png|200px|center]]  
| caption = {{#invoke:Data|getData|Example/engine|subtitle}}
| caption = {{#invoke:Data|getData|Example/engine|subtitle}}
| below    = {{#invoke:Data|getData|Example/engine|manufacturer}}


| labelstyle  = width: 60%; text-align: left;
| labelstyle  = width: 60%; text-align: left;
Line 19: Line 21:
     width: 20em;
     width: 20em;
| headerstyle  = font-weight: bold; color: black; background: #f7aa33; font-size: 18px; text-align: left;
| headerstyle  = font-weight: bold; color: black; background: #f7aa33; font-size: 18px; text-align: left;
| autoheaders = y
| captionstyle = text-align: center; font-style: italic;
| captionstyle = text-align: center; font-style: italic;


Line 59: Line 62:
|  data29  = {{#ifeq: {{#invoke:Data|getData|Example/command module|stores_research}} | true | ✔ |}}
|  data29  = {{#ifeq: {{#invoke:Data|getData|Example/command module|stores_research}} | true | ✔ |}}


| header30 = {{{auxHeader|}}}
| header30 = Engine
| data31 = {{{auxData|}}}
| data31 = {{#if: {{#invoke:Data|getData|Example/engine|modules|engine}} | {{Infobox engines/doc}} |}}
 
| header32 = Parachute
| data33 = {{#if: {{#invoke:Data|getData|Example/parachute|modules|parachute}} | {{Infobox parachute/doc}} |}}


| below    = {{#invoke:Data|getData|Example/engine|manufacturer}}
}}
}}

Revision as of 23:45, 22 December 2024

T3-ST "Default"
Example Methalox Engine
Statistics
Mass (t)0.500
SizeSM
Max Temp (K)1000
Impact Tolerance (m/s)10
Monopropellant (t)100
Electric Charge (U)200
Stores Research
Engine
Mode 1
Oxidizer
Methane
0.040 t/s
0.010 t/s
Thrust: 1 atm.42.0 kN
Thrust: Vac.88.0 kN
Isp: 1 atm.223 s
Isp: Vac.628 s
Mode 2
Oxidizer
Methane
0.040 t/s
0.010 t/s
Thrust: 1 atm.42.0 kN
Thrust: Vac.88.0 kN
Isp: 1 atm.223 s
Isp: Vac.628 s
Parachute
Semi-deployed drag400.0 kN
Deployed drag850.0 kN
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