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

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(retextured the RT-10 solid fuel booster)
(Updated information using in-game test results. Current as of 0.18.2.)
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|-
 
|-
 
!colspan=4| {{#switch:{{{1}}}
 
!colspan=4| {{#switch:{{{1}}}
−
|=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron I is 31831 kg/m3)''
+
|=''Solid Fuel Density is 5880-7500 kg/m3''
−
|ru=''Плотность твердого топлива 1273-1910 кг/м3''
+
|ru=''Плотность твердого топлива 5880-7500 кг/м3''
−
|#default=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron I fuel density is 31831 kg/m3)''
+
|#default=''Solid Fuel Density is 5880-7500 kg/m3''
 
}}
 
}}
 
!colspan=2| {{#switch:{{{1}}}
 
!colspan=2| {{#switch:{{{1}}}
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|#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
 
|#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]]
 
}}
 
}}
−
!colspan=4|
+
!colspan=5|
 
!colspan=2| {{#switch:{{{1}}}
 
!colspan=2| {{#switch:{{{1}}}
 
|=[[w:Thrust-to-weight_ratio|T/W ratio]]
 
|=[[w:Thrust-to-weight_ratio|T/W ratio]]
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|#default=[[w:Thrust-to-weight_ratio|T/W ratio]]
 
|#default=[[w:Thrust-to-weight_ratio|T/W ratio]]
 
}}
 
}}
−
!colspan=2|
+
!colspan=2| {{#switch:{{{1}}}
 +
|=[[w:Thrust-to-weight_ratio|T/W ratio]]
 +
|ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]]
 +
|#default=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
 +
}}
 +
!colspan=2| {{#switch:{{{1}}}
 +
|=[[w:Thrust-to-weight_ratio|T/W ratio]]
 +
|ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]]
 +
|#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 +
}}
 
|-
 
|-
 
! scope="col" width="60px" | {{#switch:{{{1}}}
 
! scope="col" width="60px" | {{#switch:{{{1}}}
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|ru=Пустой
 
|ru=Пустой
 
|#default=Empty
 
|#default=Empty
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=[[w:Drag_(physics)|Drag]]
 +
|ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]]
 +
|#default=Fuel (L)
 
}}
 
}}
 
! scope="col" width="60px" | {{#switch:{{{1}}}
 
! scope="col" width="60px" | {{#switch:{{{1}}}
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|=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
 
|=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
 
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время горения]] [[wikipedia:ru:Секунда|(с)]]
 
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время горения]] [[wikipedia:ru:Секунда|(с)]]
−
|#default=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
+
|#default=[[w:Atmosphere_(unit)|atm]]
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 +
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]
 +
|#default=[[w:Vacuum|vac]]
 +
}}
 +
! scope="col" width="60px" | {{#switch:{{{1}}}
 +
|=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]]
 +
|ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время горения]] [[wikipedia:ru:Секунда|(с)]]
 +
|#default=[[w:Atmosphere_(unit)|atm]]
 
}}
 
}}
 
! scope="col" width="60px" | {{#switch:{{{1}}}
 
! scope="col" width="60px" | {{#switch:{{{1}}}
 
|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 
|=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
 
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]
 
|ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]]
−
|#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]]
+
|#default=[[w:Vacuum|vac]]
 
}}
 
}}
 
|-
 
|-
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}}
 
}}
 
| 450
 
| 450
−
| 3.5
+
| 3.7475
 
| 0.5
 
| 0.5
 +
| 433
 
| 0.3
 
| 0.3
 
| 3600
 
| 3600
 
| 7
 
| 7
 
| 250
 
| 250
−
| 7.3
+
| 6.8
 
| 51.0
 
| 51.0
−
| 25
+
| 29
−
| 212
+
| 31
 +
| 225
 +
| 240
 
|-
 
|-
 
| [[Image:Rt-b20_booster-t.png|60x60px|]]
 
| [[Image:Rt-b20_booster-t.png|60x60px|]]
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| 800
 
| 800
 
| 6.75
 
| 6.75
−
| 0.75
+
| 1.75
 +
| 850
 
| 0.3
 
| 0.3
 
| 3900
 
| 3900
 
| 7
 
| 7
−
| 550
+
| 300
−
| 7.6
+
| 4.5
−
| 68.0
+
| 17.5
−
| 30
+
| 48
−
| 280
+
| 52
 +
| 230
 +
| 250
 
|-
 
|-
 
| [[Image:Sepratron 1.PNG|60x60px|]]
 
| [[Image:Sepratron 1.PNG|60x60px|]]
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}}
 
}}
 
| 100
 
| 100
 +
| 0.2175
 
| 0.15
 
| 0.15
−
| 0.05
+
| 9
 
| 0.3
 
| 0.3
 
| 3600
 
| 3600
 
| 7
 
| 7
 
| 20
 
| 20
 +
| 9.4
 
| 13.6
 
| 13.6
−
| 40.8
+
| 3
−
| 5
+
| 3
−
| 102
+
| 100
 +
| 100
 
|}
 
|}

Revision as of 02:05, 7 January 2013

Solid Fuel Density is 5880-7500 kg/m3 Mass (t) T/W ratio Burn (s) Isp (s)
Image Part Size Cost ($) Full Empty Fuel (L) Drag Max Temp (K) Tolerance Thrust (kN) Full Empty atm vac atm vac
File:Rt-10 solid fuel booster.jpg RT-10 Solid Fuel Booster Small 450 3.7475 0.5 433 0.3 3600 7 250 6.8 51.0 29 31 225 240
File:Rt-b20 booster-t.png Rockomax BACC Solid Fuel Booster Small 800 6.75 1.75 850 0.3 3900 7 300 4.5 17.5 48 52 230 250
File:Sepratron 1.PNG Sepratron I Radial Mounted 100 0.2175 0.15 9 0.3 3600 7 20 9.4 13.6 3 3 100 100
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