Difference between revisions of "Template:Stats Table Jet Engines"
From Kerbal Space Program Wiki
Kerbolnaut (talk | contribs) (Adding column to indicate which engines are capable of reversing their thrust) |
(Русский перевод, коррекция под 1.0.5) |
||
| Line 6: | Line 6: | ||
! scope="col" width="60px" | {{lang | ! scope="col" width="60px" | {{lang | ||
|en=[[Liquid fuel|Fuel]]<br>({{mark|fuelflow}}) | |en=[[Liquid fuel|Fuel]]<br>({{mark|fuelflow}}) | ||
| − | |ru=[[w:ru:Ракетное_топливо| | + | |ru=[[w:ru:Ракетное_топливо|Расход<br>топлива]]<br>({{mark|fuelflow}}) |
|pl=[[Liquid fuel/pl|Paliwo]]<br>({{mark|fuelflow}}) | |pl=[[Liquid fuel/pl|Paliwo]]<br>({{mark|fuelflow}}) | ||
|ko=[[w:ko:로켓 연료|연료]]<br>({{mark|fuelflow}}) | |ko=[[w:ko:로켓 연료|연료]]<br>({{mark|fuelflow}}) | ||
| Line 29: | Line 29: | ||
! scope="col" width="60px" | {{lang | ! scope="col" width="60px" | {{lang | ||
|en=Reverse | |en=Reverse | ||
| − | |ru= | + | |ru=Реверс |
|pl=odwracać | |pl=odwracać | ||
|ko=거꾸로 되다 | |ko=거꾸로 되다 | ||
| Line 44: | Line 44: | ||
|hr=Osnovni mlazni motor J-20 "Juno" | |hr=Osnovni mlazni motor J-20 "Juno" | ||
|hu=J-20 "Juno" Alap-Sugárhajtómű | |hu=J-20 "Juno" Alap-Sugárhajtómű | ||
| − | |ru= | + | |ru=Турбореактивный двигатель J-20 "Юнона"<br>(J-20 "Juno" Basic Jet Engine)}} |
| {{Radial Size|0}} | | {{Radial Size|0}} | ||
| 450 | | 450 | ||
| − | | {{Formatnum/SortCell|0.25| | + | | {{Formatnum/SortCell|0.25|2}} |
| {{Formatnum/SortCell|2000}} | | {{Formatnum/SortCell|2000}} | ||
| 7 | | 7 | ||
| Line 61: | Line 61: | ||
|es=Turbofan J-33 "Wheesley" | |es=Turbofan J-33 "Wheesley" | ||
|hu=J-33 "Wheesley" Sugárhajtómű | |hu=J-33 "Wheesley" Sugárhajtómű | ||
| − | |ru=Турбовентиляторный двигатель J-33 "Wheesley"}} | + | |ru=Турбовентиляторный двигатель J-33 "Уизли"<br>(J-33 "Wheesley" Turbofan Engine)}} |
| {{Radial Size|1}} | | {{Radial Size|1}} | ||
| − | | | + | | 1440 |
| {{Formatnum/SortCell|1.5|1}} | | {{Formatnum/SortCell|1.5|1}} | ||
| {{Formatnum/SortCell|2000}} | | {{Formatnum/SortCell|2000}} | ||
| Line 77: | Line 77: | ||
| {{if lang link|J-404 "Panther" Afterburning Turbofan | | {{if lang link|J-404 "Panther" Afterburning Turbofan | ||
|hu=J-404 "Panther" Utánégetős Sugárhajtómű | |hu=J-404 "Panther" Utánégetős Sugárhajtómű | ||
| − | |ru= | + | |ru=Турбовентиляторный двигатель с форсажной камерой J-404 "Пантера"<br>(J-404 "Panther" Afterburning Turbofan)}} |
| {{Radial Size|1}} | | {{Radial Size|1}} | ||
| {{Formatnum/SortCell|2000}} | | {{Formatnum/SortCell|2000}} | ||
| Line 93: | Line 93: | ||
| {{if lang link|J-X4 "Whiplash" Turbo Ramjet Engine | | {{if lang link|J-X4 "Whiplash" Turbo Ramjet Engine | ||
|hu=J-X4 "Whiplash" Turbó Torlósugár Hajtómű | |hu=J-X4 "Whiplash" Turbó Torlósugár Hajtómű | ||
| − | |ru= | + | |ru=Прямоточно-турбинный реактивный двигатель J-X4 "Кнут"<br>(J-X4 "Whiplash" Turbo Ramjet Engine)}} |
| {{Radial Size|1}} | | {{Radial Size|1}} | ||
| {{Formatnum/SortCell|2250}} | | {{Formatnum/SortCell|2250}} | ||
| Line 110: | Line 110: | ||
|es=Turbofan J-90 "Goliath" | |es=Turbofan J-90 "Goliath" | ||
|hu=J-90 "Goliath" Sugárhajtómű | |hu=J-90 "Goliath" Sugárhajtómű | ||
| − | |ru= | + | |ru=Турбовентиляторный двигатель J-90 "Голиаф"<br>(J-90 "Goliath" Turbofan Engine)}} |
| {{Radial Size|2}} | | {{Radial Size|2}} | ||
| {{Formatnum/SortCell|2600}} | | {{Formatnum/SortCell|2600}} | ||
| Line 128: | Line 128: | ||
|hr=Motor CR-7 R.A.P.I.E.R. | |hr=Motor CR-7 R.A.P.I.E.R. | ||
|hu=CR-7 R.A.P.I.E.R. Hajtómű | |hu=CR-7 R.A.P.I.E.R. Hajtómű | ||
| − | |ru= | + | |ru=Комбинированный двигатель CR-7 R.A.P.I.E.R. |
|ko=CR-7 R.A.P.I.E.R.엔진 | |ko=CR-7 R.A.P.I.E.R.엔진 | ||
}}<ref group="{{dict|Note}}">{{lang | }}<ref group="{{dict|Note}}">{{lang | ||
| Line 134: | Line 134: | ||
|de=Die R.A.P.I.E.R. Engine ist eine Kombination eines Raketentriebwerks und Jettriebwerks. Nur die Eigenschaften des Jettriebwerks werden aufgelistet. | |de=Die R.A.P.I.E.R. Engine ist eine Kombination eines Raketentriebwerks und Jettriebwerks. Nur die Eigenschaften des Jettriebwerks werden aufgelistet. | ||
|hu=A R.A.P.I.E.R. egy sugár-rakéta kettős üzemmódra tervezett speciális hajtómű. Itt csak a sugárhajtómű üzemmód alatti tulajdonságai látszódnak | |hu=A R.A.P.I.E.R. egy sugár-rakéta kettős üzemmódra tervezett speciális hajtómű. Itt csak a sugárhajtómű üzemmód alatti tulajdonságai látszódnak | ||
| − | |ru=Двигатель | + | |ru=Двигатель R.A.P.I.E.R. является комбинацией [[w:Жидкостный_ракетный_двигатель|ЖРД]] и [[w:Воздушно-реактивный_двигатель|ВРД]]. Показаны только параметры, относящиеся к ВРД. |
|ja=R.A.P.I.E.R.エンジンは液体燃料エンジンとしてもジェットエンジンとしても機能するため、本項ではジェットエンジンとしての性能のみを記載する。 | |ja=R.A.P.I.E.R.エンジンは液体燃料エンジンとしてもジェットエンジンとしても機能するため、本項ではジェットエンジンとしての性能のみを記載する。 | ||
|ko=R.A.P.I.E.R 엔진은 액체연료 엔진 모드와 제트 엔진 모드로 사용할 수 있습니다. 여기서는 제트 엔진으로써의 성능만을 기재합니다 | |ko=R.A.P.I.E.R 엔진은 액체연료 엔진 모드와 제트 엔진 모드로 사용할 수 있습니다. 여기서는 제트 엔진으로써의 성능만을 기재합니다 | ||
Revision as of 18:34, 21 February 2016
| Image | Part | Radial size | Cost (  ) |
Mass (t) |
Max. Temp. (K) |
Tolerance (m/s) |
Thrust (kN) |
TWR | Fuel (  /s)
|
Isp (s) | TVC (°) |
Reverse |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
 |
J-20 "Juno" Basic Jet Engine | Tiny | 450 | 0.25 | 2 000 | 7 | 20.0 Mach 0 20.6 Mach 1.3 |
8.15 Mach 0 8.40 Mach 1.30 |
0.064 | 6 400 | — | ✘ |
 |
J-33 "Wheesley" Turbofan Engine | Small | 1440 | 1.5 | 2 000 | 7 | 120.0 Mach 0 | 8.15 Mach 0 | 0.233 | 10 500 | — | ✔ |
 |
J-404 "Panther" Afterburning Turbofan | Small | 2 000 | 1.2 | 2 000 | 7 | 85.0 Mach 0 107.9 Mach 1.8 / 130.0 Mach 0 219.5Mach 2.5 |
7.22 Mach 0 9.16 Mach 1.8 / 11.04 Mach 0 18.64Mach 2.5 |
0.193 / 0.663 |
9 000 / 4 000 |
10.0 | ✘ |
 |
J-X4 "Whiplash" Turbo Ramjet Engine | Small | 2 250 | 1.8 | 2 000 | 7 | 130.0 Mach 0 386.7 Mach 3.0 |
7.36 Mach 0 21.90 Mach 3.0 |
0.663 | 4 000 | 1.0 | ✘ |
 |
J-90 "Goliath" Turbofan Engine | Large | 2 600 | 4.5 | 2 000 | 7 | 360.0 Mach 0 | 8.15 Mach 0 | 0.583 | 12 600 | — | ✔ |
 |
CR-7 R.A.P.I.E.R. Engine[Note 1] | Small | 6 000 | 2.0 | 2 000 | 20 | 105.0 Mach 0 892.5 Mach 3.75 |
5.35 Mach 0 45.49 Mach 3.75 |
0.446 | 3 200 | 3.0 | ✘ |
- ↑ The R.A.P.I.E.R. Engine is a combination of liquid fuel and jet engine. Only the jet engine properties are shown.
