Difference between revisions of "J-X4 "Whiplash" Turbo Ramjet Engine"
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(*difference between turbofan and turbojet are purely trivia;) |
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The TurboJet Engine can provide lots of thrust in high altitudes. At almost all altitudes it generates more thrust than the [[Basic Jet Engine]], but it has a much lower [[specific impulse]] at low altitudes. | The TurboJet Engine can provide lots of thrust in high altitudes. At almost all altitudes it generates more thrust than the [[Basic Jet Engine]], but it has a much lower [[specific impulse]] at low altitudes. | ||
| − | In real life, a [[w:Turbojet|turbojet]] engine's fan pulls all the air from the intake through a combustion chamber, as opposed to a [[w:Turbofan|turbofan]] in which some of the air sucked in bypasses the chamber and is shot out of the back without being burned at all. The turbojet is more efficient at high speeds and in thinner atmospheres, although turbofans are much quieter and are very efficient when moving slowly. This is why turbofans are almost exclusively fitted on commercial airliners, and turbojets are more common on supersonic [[plane]]s. | + | == Trivia == |
| + | The internal part's name is ''turboFanEngine'' which is another kind of jet engine. In real life, a [[w:Turbojet|turbojet]] engine's fan pulls all the air from the intake through a combustion chamber, as opposed to a [[w:Turbofan|turbofan]] in which some of the air sucked in bypasses the chamber and is shot out of the back without being burned at all. The turbojet is more efficient at high speeds and in thinner atmospheres, although turbofans are much quieter and are very efficient when moving slowly. This is why turbofans are almost exclusively fitted on commercial airliners, and turbojets are more common on supersonic [[plane]]s. | ||
== Description == | == Description == | ||
Revision as of 13:16, 4 September 2013
| J-X4 "Whiplash" Turbo Ramjet Engine | ||
 | ||
| Jet engine by C7 Aerospace Division | ||
| Radial size | Small | |
| Cost | (total) | 2 250.00 
|
| Mass | (total) | 1.800 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Hypersonic Flight
| |
| Unlock cost | 18 000
| |
| Since version | 0.15 | |
| Part configuration | jetEngineTurbo.cfg | |
| Maximum thrust | 130.00 kN | |
| Isp | (max) | 4000 s |
| Fuel consumption | 0.66  /s
| |
| Intake air consumption | 5.30  /s
| |
| Thrust vectoring | 1 ° | |
| Electricity generated | 5.0 ⚡/s | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | No | |
| On an escape | No | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
The TurboJet Engine is an air-breathing engine which requires liquid fuel from fuel tanks and intake air.
Contents
Usage
The TurboJet Engine can provide lots of thrust in high altitudes. At almost all altitudes it generates more thrust than the Basic Jet Engine, but it has a much lower specific impulse at low altitudes.
Trivia
The internal part's name is turboFanEngine which is another kind of jet engine. In real life, a turbojet engine's fan pulls all the air from the intake through a combustion chamber, as opposed to a turbofan in which some of the air sucked in bypasses the chamber and is shot out of the back without being burned at all. The turbojet is more efficient at high speeds and in thinner atmospheres, although turbofans are much quieter and are very efficient when moving slowly. This is why turbofans are almost exclusively fitted on commercial airliners, and turbojets are more common on supersonic planes.
Description
| “ | A standard air breathing engine. This model utilizes an array of rotating fins to enable limited range thrust vectoring. This engine chokes in thick atmospheres and will only operate efficiently in the thinner air, due to its high performance ram air intakes. — C7 Aerospace Division |
” |
Created by: C. Jenkins
Changes
- Initial Release
