Difference between revisions of "T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine/Box"
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m (BobBot moved page Toroidal Aerospike Rocket/Box to T-1 Toroidal "Aerospike" Liquid Fuel Engine/Box: Renamed part after update.) |
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file= | + | |file=ToroidalAerospikeLiquidFuelEngine.png |
|type=lfe | |type=lfe | ||
| − | |size= | + | |size=r |
| + | |size2=1 | ||
|manufacturer=C7 | |manufacturer=C7 | ||
|costs=3850 | |costs=3850 | ||
| − | |mass=1. | + | |mass=1.0 |
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=20 | |tolerance=20 | ||
|research=Hypersonic Flight | |research=Hypersonic Flight | ||
| − | |unlock cost= | + | |unlock cost=24500 |
|since=0.15 | |since=0.15 | ||
|filename=liquidEngineAerospike.cfg | |filename=liquidEngineAerospike.cfg | ||
|part=liquidEngineAerospike | |part=liquidEngineAerospike | ||
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust= | + | |thrust=180 |
| − | |isp-atm= | + | |isp-atm=290 |
| − | |isp-vac= | + | |isp-vac=340 |
| − | | | + | |fuel=lfox |
| − | | | + | }} |
| + | {{Infobox/Part/generator | ||
| + | |generate=5.0 | ||
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=127 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=1600 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:23, 9 October 2024
| T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by C7 Aerospace Division | ||
| Radial size | Radial mounted, Small | |
| Cost | (total) | 3 850.00 
|
| Mass | (total) | 1.000 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 20 m/s | |
| Research |  Hypersonic Flight
| |
| Unlock cost | 24 500
| |
| Since version | 0.15 | |
| Part configuration | liquidEngineAerospike.cfg | |
| Maximum thrust | (1 atm) | 153.53 kN |
| (vacuum) | 180.00 kN | |
| Isp | (1 atm) | 290 s |
| (vacuum) | 340 s | |
| Fuel consumption | 10.80  /s
| |
| Thrust vectoring | No | |
| 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 | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
| Packed volume | 1600 l | |
