Difference between revisions of "T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine/Box"
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|isp-atm=290 | |isp-atm=290 | ||
|isp-vac=340 | |isp-vac=340 | ||
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|vectoring= | |vectoring= | ||
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}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
|environments=15 | |environments=15 | ||
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Revision as of 19:01, 3 May 2015
| T-1 Toroidal Aerospike "Dart" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by C7 Aerospace Division | ||
| Radial size | Small | |
| Cost | (total) | 3 850.00 
|
| Mass | (total) | 1.500 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 | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | No | |
| In an orbit | No | |
| On an escape | No | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
