Difference between revisions of "Template:Stats Table Solid Fuel Boosters (Demo)"

Revision as of 19:35, 9 May 2015

Solid Fuel Density is 7,5 kg/unit				Mass (t)							T/W ratio		Burn (s)		Isp (s)
Image	Part	Size	Cost ()	Full	Empty	Fuel ()	Drag	Max Temp (K)	Tolerance	Thrust (kN)	Full	Empty	atm	vac	atm	vac
	RT-10 Solid Fuel Booster	Small	450	3.7475	0.5	433	0.3	3 600	7	250	6.8	51.0	29	31	225	240

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 !colspan=2| {{lang|en=[[w:Thrust-to-weight_ratio|T/W ratio]]|ru=[[w:ru:Тяговооружённость|Тяговооружённость]]|pl=[[w:pl:Współczynnik_ciągu_do_ciężaru|Współczynnik T/W]]
-|hu=[[Thrust-to-weight_ratio/hu|TWR]]
+|hu=[[Thrust-to-weight ratio/hu|TWR]]
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 !colspan=2| {{lang|en=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время<br>горения]] [[wikipedia:ru:Секунда|(с)]]|pl=
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 !colspan=2| {{lang|en=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]|ru=[[wikipedia:ru:Удельный_импульс|Удельный<br>импульс]] [[wikipedia:ru:Секунда|(с)]]|pl=[[w:pl:Impuls_właściwy|Isp]] [[w:pl:Sekunda|(s)]]
-|hu=[[Specific_impulse/hu|I<sub>sp</sub>]] [[w:hu:Másodperc|(s)]]
+|hu=[[Specific impulse/hu|I<sub>sp</sub>]] [[w:hu:Másodperc|(s)]]
 }}
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