Difference between revisions of "Parts/Propulsion"
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< Parts
(hungarian added) |
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|en=Liquid Fuel Engines | |en=Liquid Fuel Engines | ||
|fr=Moteurs à Carburant Liquide | |fr=Moteurs à Carburant Liquide | ||
− | |ru= | + | |ru=[[w:ru:Жидкостный_ракетный_двигатель|Жидкостные ракетные двигатели]] |
|pl=Silniki na paliwo ciekłe | |pl=Silniki na paliwo ciekłe | ||
− | |zh-cn=液体燃料发动机|ko=액체연료엔진 | + | |zh-cn=液体燃料发动机 |
− | |it= | + | |ko=액체연료엔진 |
+ | |it=Endoreattori | ||
|de=Raketentriebwerke für Flüssigtreibstoff | |de=Raketentriebwerke für Flüssigtreibstoff | ||
|ja=液体燃料エンジン | |ja=液体燃料エンジン | ||
|es=Motores de combustible líquido | |es=Motores de combustible líquido | ||
+ | |pt=Motores de combustível liquido | ||
|hr=Raketni motori na tekuće gorivo | |hr=Raketni motori na tekuće gorivo | ||
− | |hu=Folyékony Hajtóanyagú Rakétahajtóművek [Liquid Fuel Engines] | + | |hu=[[Liquid fuel engine/hu|Folyékony Hajtóanyagú Rakétahajtóművek]] [Liquid Fuel Engines] |
}} ==== | }} ==== | ||
+ | |||
{{Stats Table Liquid Fuel Engines}} | {{Stats Table Liquid Fuel Engines}} | ||
Line 17: | Line 20: | ||
|en=Jet Engines | |en=Jet Engines | ||
|fr=Moteurs à Réaction | |fr=Moteurs à Réaction | ||
− | |ru= | + | |ru=[[w:ru:Воздушно-реактивный двигатель|Воздушно-реактивные двигатели]] |
|pl=Silniki Odrzutowe | |pl=Silniki Odrzutowe | ||
|zh-cn=喷气发动机 | |zh-cn=喷气发动机 | ||
Line 25: | Line 28: | ||
|ja=ジェットエンジン | |ja=ジェットエンジン | ||
|es=Motores de reacción (Jet) | |es=Motores de reacción (Jet) | ||
+ | |pt= Motores de Reação | ||
|hr=Mlazni motori | |hr=Mlazni motori | ||
− | |hu=Sugárhajtóművek [Jet Engines] | + | |hu=[[Jet engine/hu|Sugárhajtóművek]] [Jet Engines] |
}} ==== | }} ==== | ||
{{Stats Table Jet Engines}} | {{Stats Table Jet Engines}} | ||
Line 33: | Line 37: | ||
|en=Solid Fuel Boosters | |en=Solid Fuel Boosters | ||
|fr=Boosters à Carburant Solide | |fr=Boosters à Carburant Solide | ||
− | |ru= | + | |ru=[[w:ru:Твердотопливный_ракетный_двигатель|Ракетные двигатели твёрдого топлива (РДТТ)]] |
|pl=Dopalacze na paliwo stałe | |pl=Dopalacze na paliwo stałe | ||
|zh-cn=固体燃料发动机 | |zh-cn=固体燃料发动机 | ||
Line 39: | Line 43: | ||
|it=Motori a carburante solido | |it=Motori a carburante solido | ||
|de=Feststoffrakete | |de=Feststoffrakete | ||
− | |ja= | + | |ja=固体燃料ブースター |
|es=Aceleradores de combustible sólido | |es=Aceleradores de combustible sólido | ||
+ | |pt=Boosters de combustível sólido | ||
|hr=Motori na kruto gorivo | |hr=Motori na kruto gorivo | ||
− | |hu=Szilárd Hajtóanyagú Gyorsítórakéták [Solid Fuel Boosters] | + | |hu=[[Solid rocket booster/hu|Szilárd Hajtóanyagú Gyorsítórakéták]] [Solid Fuel Boosters] |
}} ==== | }} ==== | ||
{{Stats Table Solid Fuel Boosters}} | {{Stats Table Solid Fuel Boosters}} | ||
Line 49: | Line 54: | ||
|en=Liquid Fuel Tanks | |en=Liquid Fuel Tanks | ||
|fr=Réservoirs à Carburant Liquide | |fr=Réservoirs à Carburant Liquide | ||
− | |ru=Баки с | + | |ru=Баки с двухкомпонентным топливом ([[Liquid_fuel/ru|жидкое топливо]] + [[Oxidizer/ru|окислитель]]) |
|pl=Zbiorniki na paliwo ciekłe | |pl=Zbiorniki na paliwo ciekłe | ||
|zh-cn=液体燃料储存罐 | |zh-cn=液体燃料储存罐 | ||
Line 55: | Line 60: | ||
|it=Serbatoi di carburante liquido | |it=Serbatoi di carburante liquido | ||
|de=Flüssigtreibstofftanks | |de=Flüssigtreibstofftanks | ||
− | |ja= | + | |ja=液体燃料タンク |
|es=Tanques de combustible líquido | |es=Tanques de combustible líquido | ||
+ | |pt=Tanques de combustível Liquido | ||
|hr=Spremnici tekućeg raketnog goriva | |hr=Spremnici tekućeg raketnog goriva | ||
− | |hu=Folyékony Hajtóanyag Tartályok [Liquid Fuel Tanks] | + | |hu=[[Liquid fuel tank/hu|Folyékony Hajtóanyag Tartályok]] [Liquid Fuel Tanks] |
}} ==== | }} ==== | ||
− | {{Stats | + | {{Stats table rocket fuel tanks}} |
==== {{lang | ==== {{lang | ||
|en=Fuselages (Jet Fuel Tanks) | |en=Fuselages (Jet Fuel Tanks) | ||
|fr=Fuselages (Réservoirs à Carburant pour Avions) | |fr=Fuselages (Réservoirs à Carburant pour Avions) | ||
− | |ru= | + | |ru=Баки с [[Liquid_fuel/ru|жидким топливом]] |
|pl=Zbiorniki na paliwo lotnicze | |pl=Zbiorniki na paliwo lotnicze | ||
|zh-cn=机身(喷气发动机燃料储存罐) | |zh-cn=机身(喷气发动机燃料储存罐) | ||
Line 71: | Line 77: | ||
|de=Flugzeugtreibstoff | |de=Flugzeugtreibstoff | ||
|es=Fuselajes (Tanques para motores jet) | |es=Fuselajes (Tanques para motores jet) | ||
+ | |pt=fuselagens ( Tanques para motores de Jatos ) | ||
+ | |ja=胴体 (ジェット燃料タンク) | ||
|hr=Trupovi (spremnici avionskog goriva) | |hr=Trupovi (spremnici avionskog goriva) | ||
|hu=Repülőgéptörzsek (Folyékony Üzemanyag Tartályok) [Fuselages] | |hu=Repülőgéptörzsek (Folyékony Üzemanyag Tartályok) [Fuselages] | ||
}} ==== | }} ==== | ||
{{lang | {{lang | ||
− | |en=Jet fuel is identical to the liquid fuel in liquid fuel tanks. | + | |en=Jet fuel is identical to the liquid fuel in liquid fuel tanks. Топливо для [[w:ru:Воздушно-реактивный_двигатель|ВРД]] идентично жидкому топливу для [[w:ru:Жидкостный_ракетный_двигатель|ЖРД]]. |
|fr=Le Carburant pour avions est identique au Carburant Liquide, mais ne contient pas d'agent oxydant, afin de rendre les fuselages plus légers. | |fr=Le Carburant pour avions est identique au Carburant Liquide, mais ne contient pas d'agent oxydant, afin de rendre les fuselages plus légers. | ||
|de=Flugzeugtreibstoff ist der selben Brennstoff wie in Flüssigtreibstofftanks. | |de=Flugzeugtreibstoff ist der selben Brennstoff wie in Flüssigtreibstofftanks. | ||
|es=El combustible para jets es idéntico al combustible líquido. | |es=El combustible para jets es idéntico al combustible líquido. | ||
+ | |pt=O combustível para jato e idêntico ao combustível liquido | ||
+ | |ja=ジェット燃料はロケット用燃料タンク内の液体燃料と同一のものである。 | ||
|hr=Avionsko gorivo u trupovima identično je segmentu tekućeg goriva u spremnicima tekućeg raketnog goriva. | |hr=Avionsko gorivo u trupovima identično je segmentu tekućeg goriva u spremnicima tekućeg raketnog goriva. | ||
|hu=Csak folyékony üzemanyagot tárolnak, oxidálószer nélkül. | |hu=Csak folyékony üzemanyagot tárolnak, oxidálószer nélkül. | ||
+ | |ko=제트 연료는 액체 연료 통의 액체 연료와 동일합니다. | ||
+ | |ru=Топливо для [[w:ru:Воздушно-реактивный_двигатель|ВРД]] идентично жидкому топливу для [[w:ru:Жидкостный_ракетный_двигатель|ЖРД]]. | ||
}} | }} | ||
− | {{Stats | + | {{Stats table liquid fuel tanks}} |
==== {{lang | ==== {{lang | ||
|en=RCS Fuel Tanks | |en=RCS Fuel Tanks | ||
|fr=Réservoirs de RCS | |fr=Réservoirs de RCS | ||
− | |ru=Баки для RCS | + | |ru=Баки с [[monopropellant/ru|монопропеллентом]] для [[RCS/ru|системы ориентации]] (RCS) |
|pl=Zbiorniki na RCS | |pl=Zbiorniki na RCS | ||
|zh-cn=RCS燃料储存罐 | |zh-cn=RCS燃料储存罐 | ||
Line 94: | Line 106: | ||
|de=RCS-Tanks | |de=RCS-Tanks | ||
|es=Tanques de combustible monopropelente (RCS) | |es=Tanques de combustible monopropelente (RCS) | ||
+ | |pt=Tanques de combustível Monopropelente (RCS) | ||
+ | |ja=RCS(姿勢制御システム)用燃料タンク | ||
|hr=Spremnici pogonskog plina za upravljačke potisnike (RCS) | |hr=Spremnici pogonskog plina za upravljačke potisnike (RCS) | ||
− | |hu=Egykomponensű Hajtóanyag Tartályok [RCS Fuel Tanks] | + | |hu=[[RCS/hu|RCS Hajtóanyag Tartályok (Egykomponensű Hajtóanyag Tartályok)]] [RCS Fuel Tanks] |
}} ==== | }} ==== | ||
{{Stats Table RCS Fuel}} | {{Stats Table RCS Fuel}} | ||
+ | |||
+ | ===={{lang | ||
+ | |en=Xenon | ||
+ | |fr=Xénon | ||
+ | |pl=Ksenon | ||
+ | |zh-cn=氙离子推进系统 | ||
+ | |ja=キセノンガスイオンエンジン | ||
+ | |ko=제논 | ||
+ | |it=Gas Xenon | ||
+ | |ru=[[Ion engine/ru|Ионный двигатель]] и его расходный материал - [[Xenon gas/ru|Ксенон]] | ||
+ | |hr=Ksenon | ||
+ | |hu=[[Ion engine/hu|Ionhajtóművek]] [Ion engine] és [[Xenon gas/hu|Xenontartályok]] | ||
+ | }}==== | ||
+ | {{Stats Table Xenon Engines}} | ||
+ | |||
+ | {{Stats Table Xenon Tanks}} |
Latest revision as of 13:11, 1 February 2023
Contents
Liquid Fuel Engines
Thrust (kN) |
T/W ratio |
Max. Fuel Consumption (/s) |
Isp (s) | TVC | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
atm | vac | atm | vac | atm | vac | Gimbal (°) | |
LV-1R "Spider" Liquid Fuel Engine | Radial mounted | 120 | 0.02 | 2 000 | 7 | 50 | 1.79 | 2.0 | 9.14 | 10.20 | 0.141 | 260 | 290 | 10.0 | |
24-77 "Twitch" Liquid Fuel Engine | Radial mounted | 230 | 0.08 | 2 000 | 7 | 50 | 15.17 | 16.0 | 19.34 | 20.39 | 1.125 | 275 | 290 | 8.0 | |
Mk-55 "Thud" Liquid Fuel Engine | Radial mounted | 820 | 0.90 | 2 000 | 7 | 50 | 108.20 | 120.0 | 12.26 | 13.60 | 8.024 | 275 | 305 | 8.0 | |
O-10 "Puff" MonoPropellant Fuel Engine[Note 1] | Radial mounted | 150 | 0.09 | 2 000 | 7 | 50 | 9.60 | 20.0 | 10.88 | 22.66 | 2.039 | 120 | 250 | 6.0 | |
LV-1 "Ant" Liquid Fuel Engine | Tiny, Radial mounted | 110 | 0.02 | 2 000 | 7 | 50 | 0.51 | 2.0 | 2.59 | 10.20 | 0.129 | 80 | 315 | — | |
48-7S "Spark" Liquid Fuel Engine | Tiny | 240 | 0.13 | 2 000 | 7 | 50 | 16.56 | 20.0 | 12.99 | 15.69 | 1.275 | 265 | 320 | 3.0 | |
LV-909 "Terrier" Liquid Fuel Engine | Small | 390 | 0.50 | 2 000 | 7 | 50 | 14.78 | 60.0 | 3.01 | 12.24 | 3.547 | 85 | 345 | 4.0 | |
LV-T30 "Reliant" Liquid Fuel Engine | Small | 1 100 | 1.25 | 2 000 | 7 | 50 | 205.16 | 240.0 | 16.74 | 19.58 | 15.789 | 265 | 310 | — | |
LV-T45 "Swivel" Liquid Fuel Engine | Small | 1 200 | 1.50 | 2 000 | 7 | 50 | 167.97 | 215.0 | 11.42 | 14.62 | 13.703 | 250 | 320 | 3.0 | |
S3 KS-25 "Vector" Liquid Fuel Engine | Small, Radial mounted | 18 000 | 4.00 | 2 000 | 22 | 50 | 936.51 | 1 000.0 | 23.87 | 25.49 | 64.745 | 295 | 315 | 10.5 | |
T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine | Small, Radial mounted | 3 850 | 1.00 | 2 000 | 20 | 50 | 153.53 | 180.0 | 15.66 | 18.35 | 10.797 | 290 | 340 | — | |
LV-N "Nerv" Atomic Rocket Motor[Note 2] | Small | 10 000 | 3.00 | 2 500 | 12 | 50 | 13.88 | 60.0 | 0.47 | 2.04 | 1.530 | 185 | 800 | — | |
RE-L10 "Poodle" Liquid Fuel Engine | Large | 1 300 | 1.75 | 2 000 | 7 | 50 | 64.29 | 250.0 | 3.75 | 14.57 | 14.568 | 90 | 350 | 4.5 | |
RE-I5 "Skipper" Liquid Fuel Engine | Large | 5 300 | 3.00 | 2 000 | 8 | 50 | 568.75 | 650.0 | 19.33 | 22.09 | 41.426 | 280 | 320 | 2.0 | |
RE-M3 "Mainsail" Liquid Fuel Engine | Large | 13 000 | 6.00 | 2 000 | 7 | 50 | 1 379.03 | 1 500.0 | 23.44 | 25.49 | 98.683 | 285 | 310 | 2.0 | |
LFB KR-1x2 "Twin-Boar" Liquid Fuel Engine[Note 3] | Large, Radial mounted | 17 000 (14 062.4) |
42.50 (10.50) |
2 000 | 20 | 50 | 1 866.67 | 2 000.0 | 4.48 (18.13) |
4.80 (19.42) |
135.964 | 280 | 300 | 1.5 | |
Kerbodyne KR-2L+ "Rhino" Liquid Fuel Engine | Extra large | 25 000 | 9.00 | 2 000 | 7 | 50 | 1 205.88 | 2 000.0 | 13.66 | 22.66 | 119.968 | 205 | 340 | 4.0 | |
S3 KS-25x4 "Mammoth" Liquid Fuel Engine | Extra large | 39 000 | 15.00 | 2 000 | 20 | 50 | 3 746.03 | 4 000.0 | 25.47 | 27.19 | 258.978 | 295 | 315 | 2.0 | |
CR-7 R.A.P.I.E.R. Engine[Note 4] | Small | 6 000 | 2.00 | 2 000 | 20 | 50 | 162.30 | 180.0 | 8.27 | 9.18 | 12.036 | 275 | 305 | 3.0 |
- ↑ Consumes monopropellant. (the density of monopropellant is less: 4kg/unit)
- ↑ Consumes liquid fuel only.
- ↑ The LFB KR-1x2 is a liquid fuel booster -- a combination of a "normal" engine and a fuel tank.
- ↑ The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the liquid fuel engine properties are shown.
Jet Engines
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
Thrust (kN) |
TWR | Fuel (/s) |
Intake (/s) |
Isp (s) | TVC (°) |
Reverse |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
J-20 "Juno" Basic Jet Engine | Tiny | 450 | 0.25 | 2 000 | 7 | 50 | 20.0 Mach 0 20.6 Mach 1.3 |
8.16 Mach 0 8.40 Mach 1.3 |
0.064 | 1.402 | 6 400 | — | No | |
J-33 "Wheesley" Turbofan Engine | Small | 1 400 | 1.5 | 2 000 | 7 | 50 | 120.0 Mach 0 | 8.16 Mach 0 | 0.233 | 29.601 | 10 500 | — | Yes | |
J-404 "Panther" Afterburning Turbofan | Small | 2 000 | 1.2 | 2 000 | 7 | 50 | 85.00 Mach 0 107.89 Mach 1.75 / 130.00 Mach 0 219.48 Mach 2.5 |
7.22 Mach 0 9.17 Mach 1.75 / 11.05 Mach 0 18.65 Mach 2.5 |
0.193 / 0.663 |
7.705 / 7.954 |
9 000 / 4 000 |
10.0 | No | |
J-X4 "Whiplash" Turbo Ramjet Engine | Small | 2 250 | 1.8 | 2 000 | 7 | 50 | 130.00 Mach 0 386.66 Mach 3.0 |
7.36 Mach 0 21.90 Mach 3.0 |
0.663 | 5.303 | 4 000 | 1.0 | No | |
J-90 "Goliath" Turbofan Engine | Radial mounted | 2 600 | 4.5 | 2 000 | 7 | 50 | 360.0 Mach 0 | 8.16 Mach 0 | 0.583 | 132.273 | 12 600 | — | Yes | |
CR-7 R.A.P.I.E.R. Engine[Note 1] | Small | 6 000 | 2.0 | 2 000 | 20 | 50 | 105.00 Mach 0 465.64 Mach 3.75 |
5.35 Mach 0 23.74 Mach 3.75 |
0.669 | 4.015 | 3 200 | 3.0 | No |
- ↑ The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.
Solid Fuel Boosters
Solid Fuel Density is 7.5 kg/unit | Mass (t) |
Fuel () |
Thrust (kN) |
TWR | Isp (s) | Burn (s) | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Full | Empty | |||||||||||||||||
Image | Part | Radial size | Cost () |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
atm | vac | atm | vac | atm | vac | atm | vac | ||
RT-5 "Flea" Solid Fuel Booster | Small, Radial mounted | 200 (116) |
1.50 | 0.45 | 2 000 | 7 | 50 | 140 | 162.91 | 192.0 | 11.07 | 13.05 | 36.92 | 43.51 | 140 | 165 | 8.8 | |
RT-10 "Hammer" Solid Fuel Booster | Small, Radial mounted | 400 (175) |
3.56 | 0.75 | 2 000 | 7 | 50 | 375 | 197.90 | 227.0 | 5.66 | 6.50 | 26.91 | 30.86 | 170 | 195 | 23.7 | |
BACC "Thumper" Solid Fuel Booster | Small, Radial mounted | 850 (358) |
7.65 | 1.50 | 2 200 | 7 | 50 | 820 | 250.00 | 300.0 | 3.33 | 4.00 | 17.00 | 20.39 | 175 | 210 | 42.2 | |
S1 SRB-KD25k "Kickback" Solid Fuel Booster | Small, Radial mounted | 2 700 (1 140) |
24.00 | 4.50 | 2 200 | 7 | 50 | 2 600 | 593.86 | 670.0 | 2.52 | 2.85 | 13.46 | 15.18 | 195 | 220 | 62.8 | |
Sepratron I | Radial mounted | 75 (70.2) |
0.0725 | 0.0125 | 2 000 | 7 | 50 | 8 | 13.79 | 18.0 | 19.40 | 25.32 | 112.51 | 146.84 | 118 | 154 | 5.0 | |
FM1 "Mite" Solid Fuel Booster | Tiny, Radial mounted | 75 (51.0) |
0.375 | 0.075 | 2 200 | 7 | 50 | 40 | 11.012 | 12.5 | 2.93 | 3.33 | 14.68 | 16.66 | 185 | 210 | 49.44 | |
F3S0 "Shrimp" Solid Fuel Booster | Tiny, Radial mounted | 150 (96.0) |
0.875 | 0.155 | 2 200 | 7 | 50 | 90 | 26.512 | 30.0 | 3.22 | 3.65 | 17.1 | 19.35 | 190 | 215 | 47.44 | |
S2-17 "Thoroughbred" Solid Fuel Booster | Large, Radial mounted | 9 000 (4 200.0) |
70.00 | 10.00 | 2 200 | 10 | 50 | 8 000 | 1 515.217 | 1 700.0 | 2.16 | 2.43 | 15.15 | 17.0 | 205 | 230 | 79.6 | |
S2-33 "Clydesdale" Solid Fuel Booster | Large, Radial mounted | 18 500 (8 660.0) |
144.00 | 21.00 | 2 200 | 10 | 50 | 16 400 | 2 948.936 | 3 300.0 | 2.05 | 2.29 | 14.04 | 15.71 | 210 | 235 | 85.9 |
Liquid Fuel Tanks
Liquid fuel and oxidizer density are both 5 kg/unit | Mass (t) |
Liquid Fuel () |
Oxidizer () | |||||||
---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) | ||
R-4 'Dumpling' External Tank | X | 50 (39.90) |
0.1238 | 0.0138 | 2 000 | 5 | 50 | 9.9 | 12.1 | |
R-11 'Baguette' External Tank | X | 50 (25.21) |
0.3038 | 0.0338 | 2 000 | 5 | 50 | 24.3 | 29.7 | |
R-12 'Doughnut' External Tank | Small | 147 (119.46) |
0.3375 | 0.0375 | 2 000 | 6 | 50 | 27 | 33 | |
Oscar-B Fuel Tank | Tiny | 70 (51.64) |
0.225 | 0.025 | 2 000 | 6 | 50 | 18 | 22 | |
FL-T100 Fuel Tank | Small | 150 (104.1) |
0.5625 | 0.0625 | 2 000 | 6 | 50 | 45 | 55 | |
FL-T200 Fuel Tank | Small | 275 (183.2) |
1.125 | 0.125 | 2 000 | 6 | 50 | 90 | 110 | |
FL-T400 Fuel Tank | Small | 500 (316.4) |
2.25 | 0.25 | 2 000 | 6 | 50 | 180 | 220 | |
FL-T800 Fuel Tank | Small | 800 (432.8) |
4.5 | 0.5 | 2 000 | 6 | 50 | 360 | 440 | |
Rockomax X200-8 Fuel Tank | Large | 800 (432.8) |
4.5 | 0.5 | 2 000 | 6 | 50 | 360 | 440 | |
Rockomax X200-16 Fuel Tank | Large | 1 550 (815.6) |
9 | 1 | 2 000 | 6 | 50 | 720 | 880 | |
Rockomax X200-32 Fuel Tank | Large | 3 000 (1 531.2) |
18 | 2 | 2 000 | 6 | 50 | 1 440 | 1 760 | |
Rockomax Jumbo-64 Fuel Tank | Large | 5 750 (2 812.4) |
36 | 4 | 2 000 | 6 | 50 | 2 880 | 3 520 | |
Kerbodyne S3-3600 Tank | Extra large | 3 250 (1 597.6) |
20.25 | 2.25 | 2 000 | 6 | 50 | 1 620 | 1 980 | |
Kerbodyne S3-7200 Tank | Extra large | 6 500 (3 195.2) |
40.5 | 4.5 | 2 000 | 6 | 50 | 3 240 | 3 960 | |
Kerbodyne S3-14400 Tank | Extra large | 13 000 (6 390.4) |
81 | 9 | 2 000 | 6 | 50 | 6 480 | 7 920 | |
Mk2 Rocket Fuel Fuselage Short | Mk2 | 750 (566.4) |
2.29 | 0.29 | 2 500 | 50 | 50 | 180 | 220 | |
Mk2 Rocket Fuel Fuselage | Mk2 | 1 450 (1 082.8) |
4.57 | 0.57 | 2 500 | 50 | 50 | 360 | 440 | |
Mk3 Rocket Fuel Fuselage Short | Mk3 | 2 500 (1 352.5) |
14.29 | 1.79 | 2 700 | 50 | 50 | 1 125 | 1 375 | |
Mk3 Rocket Fuel Fuselage | Mk3 | 5 000 (2 705) |
28.57 | 3.57 | 2 700 | 50 | 50 | 2 250 | 2 750 | |
Mk3 Rocket Fuel Fuselage Long | Mk3 | 10 000 (5 410) |
57.14 | 7.14 | 2 700 | 50 | 50 | 4 500 | 5 500 | |
C7 Brand Adapter - 2.5m to 1.25m | Small, Large | 800 (433.0) |
4.57 | 0.57 | 2 300 | 20 | 50 | 360 | 440 | |
C7 Brand Adapter Slanted - 2.5m to 1.25m | Small, Large | 800 (433.0) |
4.57 | 0.57 | 2 300 | 20 | 50 | 360 | 440 | |
Mk2 to 1.25m Adapter | Small, Mk2 | 550 (366.4) |
2.29 | 0.29 | 2 500 | 50 | 50 | 180 | 220 | |
Mk2 to 1.25m Adapter Long | Small, Mk2 | 1 050 (682.8) |
4.57 | 0.57 | 2 500 | 50 | 50 | 360 | 440 | |
Mk2 Bicoupler | Small, Mk2 x 2 | 860 (676.4) |
2.29 | 0.29 | 2 500 | 50 | 50 | 180 | 220 | |
2.5m to Mk2 Adapter | Large, Mk2 | 800 (432.8) |
4.57 | 0.57 | 2 500 | 50 | 50 | 360 | 440 | |
Mk3 to Mk2 Adapter | Mk2, Mk3 | 2 200 (1 282.0) |
11.43 | 1.43 | 2 600 | 50 | 50 | 900 | 1 100 | |
Mk3 to 2.5m Adapter | Large, Mk3 | 2 500 (1 353.0) |
14.29 | 1.79 | 2 600 | 50 | 50 | 1 125 | 1 375 | |
Mk3 to 2.5m Adapter Slanted | Large, Mk3 | 2 500 (1 353.0) |
14.29 | 1.79 | 2 600 | 50 | 50 | 1 125 | 1 375 | |
Mk3 to 3.75m Adapter | Extra large, Mk3 | 2 500 (1 353.0) |
14.29 | 1.79 | 2 600 | 50 | 50 | 1 125 | 1 375 | |
Kerbodyne ADTP-2-3 | Large, Extra large | 1 623 (246.0) |
16.88 | 1.88 | 2 000 | 6 | 50 | 1 350 | 1 650 |
Fuselages (Jet Fuel Tanks)
Jet fuel is identical to the liquid fuel in liquid fuel tanks. Топливо для ВРД идентично жидкому топливу для ЖРД.
Liquid Fuel Density is 5 kg/unit | Mass (t) |
Liquid Fuel () | |||||||
---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) | |
Engine Nacelle[Note 1] | Small | 600 (480) |
0.925 | 0.15 | 2 000 | 10 | 50 | 150 | |
Engine Pre-cooler[Note 1] | Small | 1 650 (1 618) |
0.375 | 0.15 | 2 000 | 10 | 50 | 40 | |
Mk1 Diverterless Supersonic Intake[Note 1] | Small | 720 (560) |
1.18 | 0.17 | 2 000 | 10 | 50 | 200 | |
Mk0 Liquid Fuel Fuselage | Tiny | 200 (160) |
0.275 | 0.025 | 2 000 | 10 | 50 | 50 | |
Mk1 Liquid Fuel Fuselage | Small | 550 (230) |
2.25 | 0.25 | 2 000 | 10 | 50 | 400 | |
Mk2 Liquid Fuel Fuselage Short | Mk2 | 750 (430) |
2.29 | 0.29 | 2 500 | 50 | 50 | 400 | |
Mk2 Liquid Fuel Fuselage | Mk2 | 1 450 (810) |
4.57 | 0.57 | 2 500 | 50 | 50 | 800 | |
Mk3 Liquid Fuel Fuselage Short | Mk3 | 4 300 (2 300) |
14.29 | 1.79 | 2 700 | 50 | 50 | 2 500 | |
Mk3 Liquid Fuel Fuselage | Mk3 | 8 600 (4 600) |
28.57 | 3.57 | 2 700 | 50 | 50 | 5 000 | |
Mk3 Liquid Fuel Fuselage Long | Mk3 | 17 200 (9 200) |
57.14 | 7.14 | 2 700 | 50 | 50 | 10 000 | |
NCS Adapter | Small, Tiny | 320 (256) |
0.5 | 0.1 | 2 400 | 10 | 50 | 80 | |
FAT-455 Aeroplane Main Wing[Note 2] | X | 2 800 (2 320) |
3.78 | 0.78 | 1 200 | 15 | 50 | 600 | |
Big-S Wing Strake[Note 2] | X | 1 000 (920) |
0.6 | 0.1 | 2 400 | 15 | 50 | 100 | |
Big-S Delta Wing[Note 2] | X | 3 000 (2 760) |
2.0 | 0.5 | 2 400 | 15 | 50 | 300 |
- ↑ 1.0 1.1 1.2 The Engine Nacelle, Engine Pre-cooler, and Mk1 Diverterless Supersonic Intake are a combination of air intake and liquid fuel tank. Only the tank properties are shown. They are located in the "Aerodynamic" category in the game.
- ↑ 2.0 2.1 2.2 The FAT-455 Aeroplane Main Wing, Big-S Wing Strake, and Big-S Delta Wing are a combination of lifting surface and liquid fuel tank. Only the tank properties are shown. They are located in the "Aerodynamic" category in the game.
RCS Fuel Tanks
RCS Fuel Density is 4 kg/unit | Mass (t) |
Monopropellant () | |||||||
---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) | |
FL-R20 RCS Fuel Tank | Tiny | 200 (176) |
0.10 | 0.02 | 2 000 | 12 | 50 | 20 | |
FL-R120 RCS Fuel Tank | Small | 330 (186) |
0.56 | 0.08 | 2 000 | 12 | 50 | 120 | |
FL-R750 RCS Fuel Tank | Large | 1 800 (900) |
3.4 | 0.4 | 2 000 | 12 | 50 | 750 | |
Mk2 Monopropellant Tank | Mk2 | 750 (270) |
1.89 | 0.29 | 2 500 | 50 | 50 | 400 | |
Mk3 Monopropellant Tank | Mk3 | 5 040 (2 520) |
9.8 | 1.4 | 2 700 | 50 | 50 | 2 100 | |
Stratus-V Roundified Monopropellant Tank | X | 200 (176) |
0.10 | 0.02 | 2 000 | 12 | 50 | 20 | |
Stratus-V Cylindrified Monopropellant Tank | X | 250 (190) |
0.23 | 0.03 | 2 000 | 12 | 50 | 50 |
Xenon
Thrust (kN) |
TWR | Isp (s) | Max. Consumption | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
atm | vac | atm | vac | atm | vac | Electricity (⚡/s) |
Xenon (/s) |
IX-6315 "Dawn" Electric Propulsion System | Tiny | 8 000 | 0.25 | 2 000 | 7 | 50 | 0.048 | 2.0 | 0.019 | 0.816 | 100 | 4 200 | 8.741 | 0.486 |
Xenon density is 0.1 kg/unit | Mass (t) |
Xenon () | |||||||
---|---|---|---|---|---|---|---|---|---|
Image | Part | Radial size | Cost () |
Full | Empty | Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) | |
PB-X50R Xenon Container | Radial mounted | 2 220 (600) |
0.054 | 0.014 | 2 000 | 12 | 50 | 405 | |
PB-X150 Xenon Container | Tiny | 3 680 (800) |
0.100 | 0.024 | 2 000 | 6 | 50 | 720 | |
PB-X750 Xenon Container | Small | 24 300 (1 500) |
0.76 | 0.19 | 2 000 | 6 | 50 | 5 700 |