Difference between revisions of "User:JiminP"
From Kerbal Space Program Wiki
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[[Image:All-parts-rocket-0.8.5.png|right|thumb|버전 0.8.5에 있는 기본 부품들을 보여주는 3단 로켓]] | [[Image:All-parts-rocket-0.8.5.png|right|thumb|버전 0.8.5에 있는 기본 부품들을 보여주는 3단 로켓]] | ||
− | 이 페이지는 제일 최근 유료 버전(현재 0.17.1)의 [[Kerbal Space Program]]에 포함되어 있는 로켓 '''부품'''들의 | + | 이 페이지는 제일 최근 유료 버전(현재 0.17.1)의 [[Kerbal Space Program]]에 포함되어 있는 로켓 '''부품'''들의 목록이다. 이 부품들은 '''바닐라 부품''', '''기본 부품''' 등으로 불린다. |
− | 데모 버전의 KSP에 있는 모든 부품의 | + | 데모 버전의 KSP에 있는 모든 부품의 목록은 [[Demo Parts/ko|데모 부품]] 항목에 있다. |
+ | 게임 안에서 [[Space Plane Hangar/ko|우주 비행기 조립실]]과 [[Vehicle Assembly Building/ko|로켓 조립실]]에서 쓰이는 부품들을 7개의 분류로 나눠놨지만, 두 개의 분류에는 아직 어떠한 부품도 없다. 부품이 있는 다섯 개의 항목은 [[Parts/Command Pods/ko|사령실]], [[Parts/Propulsion/ko|추친체]], [[Parts/Commmand & Control/ko|제어부]], [[Parts/Structual & Aerodynamic/ko|구조물 및 비행체]], 그리고 [[Parts/Utility & Scientific/ko|유용한 것들 & 과학 장비]] 항목이다. | ||
− | 게임 | + | =측정 단위= |
+ | *질량과 추력의 단위가 게임 내에서 적혀있지 않지만, 질량의 단위가 [[w:Metric_tonne|톤(t)]]이며 추력의 단위가 [[w:Newton_(unit)#Common_use_of_kilonewtons_in_construction|킬로뉴턴(kN)]]이라는 것을 쉽게 알 수 있다. | ||
− | + | *커빈 해수면에서의 [[w:Thrust-to-weight_ratio|추력 대 중량비]]는, 액체 또는 고체 엔진일 경우에는 다음 공식에 의해서 계산된다. (제트 엔진은 더 복잡한 공식을 사용한다.) | |
− | |||
− | |||
− | *[[w:Thrust-to-weight_ratio| | ||
:<math>\frac{T}{W}=\frac{T\ \mathrm{kN}}{(m\ \mathrm{t})(g_{\rm 0})}</math> | :<math>\frac{T}{W}=\frac{T\ \mathrm{kN}}{(m\ \mathrm{t})(g_{\rm 0})}</math> | ||
− | + | 여기서: | |
− | :<math>T</math> | + | :<math>T</math>는 엔진 추력을 킬로뉴턴 단위로 나타낸 것이다. |
− | :<math>W</math> | + | :<math>W</math>는 [[Kerbin/ko|커빈]]의 해수면에서 엔진의 무게를 나타낸 것이다. |
− | :<math>m</math> | + | :<math>m</math>은 톤 단위로 나타낸 엔진의 질량이다. |
− | :<math>g_{\rm 0}</math> | + | :<math>g_{\rm 0}</math>은 m/s² 단위로 나타낸 커빈 해수면에서의 중력 가속도이다. (≈9.807 m/s²) |
*Specific impulse at sea level on Kerbin is is calculated by the following equation. To reduce confusion, [[w:Specific_impulse|specific impulse]] is given in both velocity and time units. Please see the discussion page for further reading on ways of expressing specific impulse. | *Specific impulse at sea level on Kerbin is is calculated by the following equation. To reduce confusion, [[w:Specific_impulse|specific impulse]] is given in both velocity and time units. Please see the discussion page for further reading on ways of expressing specific impulse. |
Revision as of 17:31, 30 November 2012
Hi
EN ⇒ KO
이 페이지는 제일 최근 유료 버전(현재 0.17.1)의 Kerbal Space Program에 포함되어 있는 로켓 부품들의 목록이다. 이 부품들은 바닐라 부품, 기본 부품 등으로 불린다.
데모 버전의 KSP에 있는 모든 부품의 목록은 데모 부품 항목에 있다.
게임 안에서 우주 비행기 조립실과 로켓 조립실에서 쓰이는 부품들을 7개의 분류로 나눠놨지만, 두 개의 분류에는 아직 어떠한 부품도 없다. 부품이 있는 다섯 개의 항목은 사령실, 추친체, 제어부, 구조물 및 비행체, 그리고 유용한 것들 & 과학 장비 항목이다.
Contents
측정 단위
- 커빈 해수면에서의 추력 대 중량비는, 액체 또는 고체 엔진일 경우에는 다음 공식에 의해서 계산된다. (제트 엔진은 더 복잡한 공식을 사용한다.)
여기서:
- 는 엔진 추력을 킬로뉴턴 단위로 나타낸 것이다.
- 는 커빈의 해수면에서 엔진의 무게를 나타낸 것이다.
- 은 톤 단위로 나타낸 엔진의 질량이다.
- 은 m/s² 단위로 나타낸 커빈 해수면에서의 중력 가속도이다. (≈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).
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 |
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
Parts/Structural & Aerodynamic