Difference between revisions of "Parts/pl"
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= Moduły Załogowe = | = Moduły Załogowe = | ||
− | {{Template:Stats Table Command Pods|{{Template:SUBPAGENAME}}}} | + | {{Template:Stats Table Command Pods/pl|{{Template:SUBPAGENAME}}}} |
= Napędy = | = Napędy = |
Revision as of 20:44, 2 November 2012
Ta strona zawiera listę wszystkich części dostępnych wraz z najnowszą płatną wersją Kerbal Space Program (obecnie 0.17.1). Części te nazywane są też oryginalnymi lub domyślnymi.
Dla listy części dostępnych wraz z wersją Demo gry przejdź tutaj.
Gra dzieli wszystkie części na 7 kategorii widocznych jako zakładki w Hangarze wahadłowców i Hangarze rakietowym, chociaż dwie z tych zakładek są obecnie nieużywane. Pozostałe pięć to Moduły Załogowe, Napędy, Dowodzenie i Kontrola, Strukturalne i Aeronautyczne, oraz Użytkowe i Naukowe.
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).
Moduły Załogowe
Template:Stats Table Command Pods/pl
Napędy
Silniki na paliwo ciekłe
Ciąg (kN) |
Współczynnik T/W |
Paliwo (/s) |
Isp (s) | TVC | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | atm | vac | atm | vac | atm | vac | Gimbal (°) | |
LV-1R "Spider" Liquid Fuel Engine | Montowany promieniowo | 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 | Montowany promieniowo | 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 | Montowany promieniowo | 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] | Montowany promieniowo | 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 | Bardzo mały, Montowany promieniowo | 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 | Bardzo mały | 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 | Mały | 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 | Mały | 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 | Mały | 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 | Mały, Montowany promieniowo | 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 | Mały, Montowany promieniowo | 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] | Mały | 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 | Duży | 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 | Duży | 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 | Duży | 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] | Duży, Montowany promieniowo | 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] | Mały | 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.
Silniki Odrzutowe
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | Ciąg (kN) |
TWR | Paliwo (/s) |
Intake (/s) |
Isp (s) | TVC (°) |
Odwracać |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
J-20 "Juno" Basic Jet Engine | Bardzo mały | 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 | Mały | 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 | Mały | 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 | Mały | 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 | Montowany promieniowo | 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] | Mały | 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.
Dopalacze na paliwo stałe
Gęstość paliwa stałego wynosi 7500 kg/m3 - (W przypadku Sepratron I to 7500 kg/m3) | Masa (t) |
Paliwo () |
Ciąg (kN) |
TWR | Isp (s) | Spalanie (s) | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Pełny | Pusty | |||||||||||||||||
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Pełny | Pusty | Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | atm | vac | atm | vac | atm | vac | atm | vac | ||
RT-5 "Flea" Solid Fuel Booster | Mały, Montowany promieniowo | 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 | Mały, Montowany promieniowo | 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 | Mały, Montowany promieniowo | 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 | Mały, Montowany promieniowo | 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 | Montowany promieniowo | 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 | Bardzo mały, Montowany promieniowo | 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 | Bardzo mały, Montowany promieniowo | 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 | Duży, Montowany promieniowo | 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 | Duży, Montowany promieniowo | 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 |
Zbiorniki na paliwo ciekłe
Gęstość paliwa rakietowego wynosi 5000 kg/m³ | Masa (t) |
Paliwo () |
Utleniacz () | |||||||
---|---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Pełny | Pusty | Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | ||
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 | Mały | 147 (119,46) |
0,3375 | 0,0375 | 2 000 | 6 | 50 | 27 | 33 | |
Oscar-B Fuel Tank | Bardzo mały | 70 (51,64) |
0,225 | 0,025 | 2 000 | 6 | 50 | 18 | 22 | |
FL-T100 Fuel Tank | Mały | 150 (104,1) |
0,5625 | 0,0625 | 2 000 | 6 | 50 | 45 | 55 | |
FL-T200 Fuel Tank | Mały | 275 (183,2) |
1,125 | 0,125 | 2 000 | 6 | 50 | 90 | 110 | |
FL-T400 Fuel Tank | Mały | 500 (316,4) |
2,25 | 0,25 | 2 000 | 6 | 50 | 180 | 220 | |
FL-T800 Fuel Tank | Mały | 800 (432,8) |
4,5 | 0,5 | 2 000 | 6 | 50 | 360 | 440 | |
Rockomax X200-8 Fuel Tank | Duży | 800 (432,8) |
4,5 | 0,5 | 2 000 | 6 | 50 | 360 | 440 | |
Rockomax X200-16 Fuel Tank | Duży | 1 550 (815,6) |
9 | 1 | 2 000 | 6 | 50 | 720 | 880 | |
Rockomax X200-32 Fuel Tank | Duży | 3 000 (1 531,2) |
18 | 2 | 2 000 | 6 | 50 | 1 440 | 1 760 | |
Rockomax Jumbo-64 Fuel Tank | Duży | 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 | Mały, Duży | 800 (433,0) |
4,57 | 0,57 | 2 300 | 20 | 50 | 360 | 440 | |
C7 Brand Adapter Slanted - 2.5m to 1.25m | Mały, Duży | 800 (433,0) |
4,57 | 0,57 | 2 300 | 20 | 50 | 360 | 440 | |
Mk2 to 1.25m Adapter | Mały, Mk2 | 550 (366,4) |
2,29 | 0,29 | 2 500 | 50 | 50 | 180 | 220 | |
Mk2 to 1.25m Adapter Long | Mały, Mk2 | 1 050 (682,8) |
4,57 | 0,57 | 2 500 | 50 | 50 | 360 | 440 | |
Mk2 Bicoupler | Mały, Mk2 x 2 | 860 (676,4) |
2,29 | 0,29 | 2 500 | 50 | 50 | 180 | 220 | |
2.5m to Mk2 Adapter | Duży, 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 | Duży, Mk3 | 2 500 (1 353,0) |
14,29 | 1,79 | 2 600 | 50 | 50 | 1 125 | 1 375 | |
Mk3 to 2.5m Adapter Slanted | Duży, 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 | Duży, Extra large | 1 623 (246,0) |
16,88 | 1,88 | 2 000 | 6 | 50 | 1 350 | 1 650 |
Zbiorniki na paliwo lotnicze
Jet fuel is identical to the liquid fuel in liquid fuel tanks. Топливо для ВРД идентично жидкому топливу для ЖРД.
Gęstość paliwa lotniczego wynosi 4000-6000 kg/m3 | Masa (t) |
Paliwo () | |||||||
---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Pełny | Pusty | Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | |
Engine Nacelle[Note 1] | Mały | 600 (480) |
0,925 | 0,15 | 2 000 | 10 | 50 | 150 | |
Engine Pre-cooler[Note 1] | Mały | 1 650 (1 618) |
0,375 | 0,15 | 2 000 | 10 | 50 | 40 | |
Mk1 Diverterless Supersonic Intake[Note 1] | Mały | 720 (560) |
1,18 | 0,17 | 2 000 | 10 | 50 | 200 | |
Mk0 Liquid Fuel Fuselage | Bardzo mały | 200 (160) |
0,275 | 0,025 | 2 000 | 10 | 50 | 50 | |
Mk1 Liquid Fuel Fuselage | Mały | 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 | Mały, Bardzo mały | 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.
Zbiorniki na RCS
Gęstość paliwa RCS wynosi 2000-2272.73 kg/m3 | Masa (t) |
Paliwo () | |||||||
---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Pełny | Pusty | Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | |
FL-R20 RCS Fuel Tank | Bardzo mały | 200 (176) |
0,10 | 0,02 | 2 000 | 12 | 50 | 20 | |
FL-R120 RCS Fuel Tank | Mały | 330 (186) |
0,56 | 0,08 | 2 000 | 12 | 50 | 120 | |
FL-R750 RCS Fuel Tank | Duży | 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 |
Ksenon
Ciąg (kN) |
TWR | Isp (s) | Max. Consumption | |||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | atm | vac | atm | vac | atm | vac | [[Electric charge/pl | Elektryczność]] (⚡/s) |
ksenon (/s) |
IX-6315 "Dawn" Electric Propulsion System | Bardzo mały | 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 | Masa (t) |
ksenon () | |||||||
---|---|---|---|---|---|---|---|---|---|
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Pełny | Pusty | Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | |
PB-X50R Xenon Container | Montowany promieniowo | 2 220 (600) |
0,054 | 0,014 | 2 000 | 12 | 50 | 405 | |
PB-X150 Xenon Container | Bardzo mały | 3 680 (800) |
0,100 | 0,024 | 2 000 | 6 | 50 | 720 | |
PB-X750 Xenon Container | Mały | 24 300 (1 500) |
0,76 | 0,19 | 2 000 | 6 | 50 | 5 700 |
Dowodzenie i Kontrola
Moduły SAS
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | S.A.S. level |
Elektryczność (⚡/s) |
---|---|---|---|---|---|---|---|---|---|
CH-J3 Fly-By-Wire Avionics Hub | Bardzo mały | 5 200 | 0,08 | 2 400 | 7 | 50 | 3 | 0,03 |
Reaction wheels
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | Torque (kN·m) |
Elektryczność (⚡/s) |
---|---|---|---|---|---|---|---|---|---|
Small Inline Reaction Wheel | Bardzo mały | 600 | 0,05 | 2 000 | 9 | 50 | 5 | 0,25 (15 ⚡/min) | |
Advanced Inline Stabilizer | Mały | 1 200 | 0,1 | 2 000 | 9 | 50 | 15 | 0,45 (27 ⚡/min) | |
Advanced Reaction Wheel Module, Large | Duży | 2 100 | 0,2 | 2 000 | 9 | 50 | 30 | 0,6 (36 ⚡/min) |
Dysze RCS
Obrazek | Nazwa Części | Rozmiar | Koszt () |
Masa (t) |
Maks. Temperatura (K) |
Tolerancja (m/s) |
Tolerancja | Ciąg (kN) |
Fuel (/s) |
Isp (s) (atm) | Isp (s) (vac) |
---|---|---|---|---|---|---|---|---|---|---|---|
RV-1X Variable Thruster Block | Montowany promieniowo | 30 | 0,005 | 1 500 | 12 | 50 | 0,1 | 0,01 | 100 | 240 | |
Place Anywhere 1 Linear RCS Port | Montowany promieniowo | 15 | 0,001 | 1 500 | 12 | 50 | 0,2 | 0,02 | 100 | 240 | |
RV-105 RCS Thruster Block | Montowany promieniowo | 45 | 0,04 | 1 500 | 15 | 50 | 1,0 | 0,11 | 100 | 240 | |
Place-Anywhere 7 Linear RCS Port | Montowany promieniowo | 25 | 0,02 | 2 600 | 15 | 50 | 2,0 | 0,21 | 100 | 240 | |
Vernor Engine[Note 1] | Montowany promieniowo | 150 | 0,08 | 2 000 | 15 | 50 | 12,0 | 0,94 | 140 | 260 |
- ↑ The Vernor Engine uses a liquid fuel/oxidizer mixture.
Strukturalne i Aeronautyczne
Parts/Structural & Aerodynamic