Template:Infobox part/doc: Difference between revisions

T3-ST "Default"
	Example Methalox Engine
Statistics
Mass (t)	0.500
Size	SM
Max Temp (K)	1000
Impact Tolerance (m/s)	10
Monopropellant (t)	100
Electric Charge (U)	200
Stores Research	✔
Engine
Oxidizer; Methane;
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
Engine Gimbal
Pitch
Pitch	2 kN
Yaw	2 kN
Generator
Output
Output	20.250 U/s
Always Active	✔
Engine Alternator	✔
Output Decays	21 y 360 d 04 h 20 m 10 s
Converter
Hydrogen (t); Methane (t);
Mode 1
Hydrogen (t); Methane (t);
Inputs
Hydrogen (t); Methane (t);	1; 1;
Outputs
Solid Fuel (t);	2;
Mode 2
Hydrogen (t);
Inputs
Hydrogen (t);	8;
Outputs
Xenon (t);	1;
Parachute
Semi-deployed drag
Semi-deployed drag	400.0 kN
Deployed drag	850.0 kN
Science Experiment
Experiment
Experiment	Crew Observation
Reports Create	Samples ✔ ; Data ✗
Report Size	5 KiB
Requirements	All situations and locations
Crew Required	1
	Community Conglomerate
	v; t; e;

Revision as of 05:57, 25 December 2024

@@ Line 70: / Line 70: @@
 | header34 = Generator
 | data35 = {{#if: {{#invoke:Data|getData|Example/engine|modules|generator}} | {{Infobox generator/doc}} |}}
+| header36 = Converter
+| data37   = {{#if: {{#invoke:Data|getData|Example/converter|modules|converter}} | {{Infobox converter/doc}} |}}
 | header80 = Parachute