Difference between revisions of "Parts"
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[[Image:All-parts-rocket-0.8.5.png|right|thumb|A three-stage rocket featuring each of the default parts as of 0.8.5]] | [[Image:All-parts-rocket-0.8.5.png|right|thumb|A three-stage rocket featuring each of the default parts as of 0.8.5]] | ||
− | This page lists the rocket '''parts''' that are included with the latest paid version of [[Kerbal Space Program]], currently 0.17. These parts are also called '''vanilla parts''', '''default parts''', and '''stock parts'''. | + | This page lists the rocket '''parts''' that are included with the latest paid version of [[Kerbal Space Program]], currently 0.17.1. These parts are also called '''vanilla parts''', '''default parts''', and '''stock parts'''. |
For a list of all the parts available in the demo version of Kerbal Space Program, look at the [[Demo Parts|demo parts]] page. | For a list of all the parts available in the demo version of Kerbal Space Program, look at the [[Demo Parts|demo parts]] page. |
Revision as of 07:54, 15 November 2012
This page lists the rocket parts that are included with the latest paid version of Kerbal Space Program, currently 0.17.1. These parts are also called vanilla parts, default parts, and stock parts.
For a list of all the parts available in the demo version of Kerbal Space Program, look at the demo parts page.
The game separates parts into seven categories for use within the Space Plane Hanger and the Vehicle Assembly Building, though two of these categories are currently unused. The five that can be selected from are Command Pods, Propulsion, Command & Control, Structural & Aerodynamic, and Utility & Scientific.
Contents
Units of measure
- While units of mass and thrust are not specifically labeled in-game, a bit of logic can quickly determine that thrust is measured in kilonewtons (kN) and mass in metric tons (t). For example, if measured in kilograms(kg), a "9 kg" Rockomax X200-16 Fuel Tank on Kerbin, having a surface gravity of 9.81 m/s2, would be roughly the size of a 48 oz coffee tin and only hold about 1.5 L of fuel. If measured in metric tons, a 9 t Rockomax X200-16 Fuel Tank under the same gravity would be about 0.67 m tall and 2 m in diameter, easily capable of holding the advertised 1600 L of fuel. Only a rocket engine with a thrust around 100 kN could have any chance to lift a 9 t fuel tank.
- Thrust to weight ratio at sea level on Kerbin is calculated by the following equation, which applies only to liquid or solid fuel rocket engines, jet engines use a complicated formula on a vehicle to vehicle basis.
where:
- is the thrust is the thrust obtained from the engine, in kilonewtons.
- is the weight of the engine at sea level on Kerbin's surface.
- is the mass of the engine in metric tons (t).
- is the acceleration at sea level on Kerbin's surface, in m/s² (≈9.807 m/s²).
- Specific impulse at sea level on Kerbin is is calculated by the following equation. To reduce confusion, specific impulse is given in both velocity and time units. Please see the discussion page for further reading on ways of expressing specific impulse.
where:
- is the specific impulse measured in seconds.
- is the thrust obtained from the engine, in kilonewtons.
- is the mass flow rate in kg/s, which is negative the time-rate of change of the vehicle's mass since propellant is being expelled.
- is the acceleration at sea level on Kerbin's surface, in m/s² (≈9.807 m/s²).
Command Pods
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
Torque (kN · m) |
S.A.S. level |
Required Crew/ Power |
Capacity (⚡) |
---|---|---|---|---|---|---|---|---|---|---|---|
Mk1 Cockpit | Small | 1 250 (1 241) |
1.28 (1.25) |
2 000 (1 100) |
40 | 50 | 10 | [Note 1] | 50 ⚡ 7.5 MP | ||
Mk1 Inline Cockpit | Small | 1 600 (1 591) |
1.03 (1.00) |
2 000 (1 100) |
40 | 50 | 10 | [Note 1] | 50 ⚡ 7.5 MP | ||
Mk2 Cockpit | Mk2 | 3 500 (3 482) |
2.06 (2.00) |
2 500 (1 400) |
45 | 50 | 15 | [Note 1] | + | 150 ⚡ 15 MP | |
Mk2 Inline Cockpit | Mk2 | 3 500 (3 470) |
2.10 (2.00) |
2 500 (1 400) |
45 | 50 | 15 | [Note 1] | + | 150 ⚡ 25 MP | |
Mk3 Cockpit | Mk3, Small | 10 000 (9 880) |
3.90 (3.50) |
2 700 (1 500) |
50 | 50 | 40/40/20[Note 2] | [Note 1] | + | 500 ⚡ 100 MP | |
Mk1 Command Pod | Small, Tiny | 600 (588) |
0.84 (0.80) |
2 200 (1 200) |
14 | 50 | 5 | [Note 1] | 50 ⚡ 10 MP | ||
Mk1-3 Command Pod | Large, Small | 3 800 (3 764) |
2.72 (2.60) |
2 400 (1 400) |
45 | 50 | 15 | [Note 1] | + | 150 ⚡ 30 MP | |
Mk1 Lander Can | Small | 1 500 (1 482) |
0.66 (0.60) |
2 000 (1 000) |
8 | 50 | 3 | [Note 1] | 50 ⚡ 15 MP | ||
Mk2 Lander Can | Large | 3 250 (3 202) |
1.515 (1.355) |
2 000 (1 200) |
8 | 50 | 15 | [Note 1] | + | 100 ⚡ 40 MP | |
PPD-12 Cupola Module | Large, Small | 3 200 (3 188) |
1.80 (1.76) |
2 000 (1 000) |
8 | 50 | 9 | [Note 1] | 200 ⚡ 10 MP | ||
EAS-1 External Command Seat | Radial mounted | 200 | 0.05 | 1 200 | 6 | 50 | — | [Note 1] | — | ||
Probodobodyne RoveMate | Small | 800 | 0.15 | 1 200 | 12 | 50 | — | 0 | 2.4 ⚡/min (144 ⚡/h) |
120 ⚡ | |
Probodobodyne QBE | Tiny | 360 | 0.07 | 1 200 | 15 | 50 | — | 0 | 1.5 ⚡/min (90 ⚡/h) |
5 ⚡ | |
Probodobodyne HECS | Tiny | 650 | 0.1 | 1 200 | 12 | 50 | 0.5 | 1 | 1.5 ⚡/min (90 ⚡/h) |
10 ⚡ | |
Probodobodyne OKTO | Tiny | 450 | 0.1 | 1 200 | 12 | 50 | 0.3 | 0 | 1.2 ⚡/min (72 ⚡/h) |
10 ⚡ | |
Probodobodyne OKTO2 | Tiny | 1 480 | 0.04 | 1 200 | 12 | 50 | — | 2 | 1.8 ⚡/min (108 ⚡/h) |
5 ⚡ | |
Probodobodyne Stayputnik | Tiny | 300 | 0.05 | 1 800 | 12 | 50 | — | — | 1.67 ⚡/min (100 ⚡/h) |
10 ⚡ | |
Probodobodyne HECS2 | Small | 7 500 | 0.2 | 2 000 | 8 | 50 | 10 | 3 | 3.0 ⚡/min (180 ⚡/h) |
1 000 ⚡ | |
RC-001S Remote Guidance Unit | Small | 2 250 | 0.1 | 2 000 | 9 | 50 | 0.5 | 3 | 3.0 ⚡/min (180 ⚡/h) |
15 ⚡ | |
RC-L01 Remote Guidance Unit | Large | 3 400 | 0.5 | 2 000 | 9 | 50 | 1.5 | 3 | 4.8 ⚡/min (288 ⚡/h) |
30 ⚡ | |
MK2 Drone Core | Mk2 | 2 700 | 0.2 | 2 500 | 20 | 50 | 15/3/3[Note 2] | 3 | 3.0 ⚡/min (180 ⚡/h) |
250 ⚡ | |
MPO Probe | Small | 9 900 (9 854) |
0.895 (0.395) |
2 200 | 9 | 50 | 6 | 3 | 3.0 ⚡/min (180 ⚡/h) |
1 000 ⚡ 45 LF 55 O | |
MTM Stage | Small | 21 500 (6 300) |
0.795 (0.415) |
2 200 | 12 | 50 | 12 | 2 | 1.8 ⚡/min (108 ⚡/h) |
4 000 ⚡ 3 800 XE |
- ↑ 1.00 1.01 1.02 1.03 1.04 1.05 1.06 1.07 1.08 1.09 1.10 In the "Career" mode in manned command modules, the performance and functionality of the SAS is determined by the presence of at least one kerbonaut with the specialization "Pilot" and the level of his specialization. In the "Science" and "Sandbox" modes, a kerbonaut with any specialization can use all the functionality of the SAS on board the manned command module without restrictions.
- ↑ 2.0 2.1 Torque differs between axes. These numbers are for pitch/yaw/roll respectively.
Propulsion
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 |
Command & Control
SAS modules
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
S.A.S. level |
Electricity (⚡/s) |
---|---|---|---|---|---|---|---|---|---|
CH-J3 Fly-By-Wire Avionics Hub | Tiny | 5 200 | 0.08 | 2 400 | 7 | 50 | 3 | 0.03 |
Reaction wheels
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
Torque (kN·m) |
Electricity (⚡/s) |
---|---|---|---|---|---|---|---|---|---|
Small Inline Reaction Wheel | Tiny | 600 | 0.05 | 2 000 | 9 | 50 | 5 | 0.25 (15 ⚡/min) | |
Advanced Inline Stabilizer | Small | 1 200 | 0.1 | 2 000 | 9 | 50 | 15 | 0.45 (27 ⚡/min) | |
Advanced Reaction Wheel Module, Large | Large | 2 100 | 0.2 | 2 000 | 9 | 50 | 30 | 0.6 (36 ⚡/min) |
RCS thrusters
Image | Part | Radial size | Cost () |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Tolerance (g) |
Thrust (kN) |
Fuel (/s) |
Isp (s) (atm) | Isp (s) (vac) |
---|---|---|---|---|---|---|---|---|---|---|---|
RV-1X Variable Thruster Block | Radial mounted | 30 | 0.005 | 1 500 | 12 | 50 | 0.1 | 0.01 | 100 | 240 | |
Place Anywhere 1 Linear RCS Port | Radial mounted | 15 | 0.001 | 1 500 | 12 | 50 | 0.2 | 0.02 | 100 | 240 | |
RV-105 RCS Thruster Block | Radial mounted | 45 | 0.04 | 1 500 | 15 | 50 | 1.0 | 0.11 | 100 | 240 | |
Place-Anywhere 7 Linear RCS Port | Radial mounted | 25 | 0.02 | 2 600 | 15 | 50 | 2.0 | 0.21 | 100 | 240 | |
Vernor Engine[Note 1] | Radial mounted | 150 | 0.08 | 2 000 | 15 | 50 | 12.0 | 0.94 | 140 | 260 |
- ↑ The Vernor Engine uses a liquid fuel/oxidizer mixture.
Structural & Aerodynamic
Parts/Structural & Aerodynamic