Difference between revisions of "Launch Escape System/Box"
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(Created page with "<noinclude>{{Data template used}}</noinclude> {{Infobox/Part |file= |role=Launch escape system |parent= |manufacturer=KD |size=s |costs=800 |mass=1 |sf=15 |drag=0.3 |temp=3900...") |
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file= | + | |file=Launch_Escape_System.png |
| − | | | + | |type=les |
| − | | | + | |size=1 |
|manufacturer=KD | |manufacturer=KD | ||
| − | + | |costs=1000 | |
| − | |costs= | + | |mass=0.9 |
| − | |mass= | + | |sf=30 |
| − | |sf= | + | |drag=0.2-0.3 |
| − | |drag=0.3 | + | |temp=2700 |
| − | |temp= | ||
|tolerance=15 | |tolerance=15 | ||
| − | |research= | + | |research=Landing |
| + | |unlock cost=4500 | ||
|since=0.23.5 | |since=0.23.5 | ||
| − | |part= | + | |filename=part.cfg |
| + | |part=launchEscapeSystem | ||
| + | |parent=Utility | ||
|more={{Infobox/Part/solid fuel engine | |more={{Infobox/Part/solid fuel engine | ||
| − | |thrust=750 | + | |thrust=750 |
| − | |fuel= | + | |isp-atm=160 |
| − | | | + | |isp-vac=180 |
| − | | | + | |fuel=30 |
| + | }} | ||
| + | {{Infobox/Part/test subject | ||
| + | |environments=255 <!-- bug in part config, so use default value --> | ||
| + | |event=n | ||
| + | |staging=y | ||
| + | }} | ||
| + | {{Infobox/Part/cargo | ||
| + | |volume=-1 | ||
| + | |stack=1 | ||
| + | }} | ||
| + | {{Infobox/Part/tank | ||
| + | |sf=30 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 07:33, 16 October 2024
| Launch Escape System | ||
 | ||
| Launch Escape System by Kerbodyne | ||
| Radial size | Small | |
| Cost | (total) | 1 000.00 
|
| (dry) | 982.00
| |
| Mass | (total) | 1.125 t |
| (dry) | 0.900 t | |
| Drag | 0.2-0.3 | |
| Max. Temp. | 2700 K | |
| Impact Tolerance | 15 m/s | |
| Research |  Landing
| |
| Unlock cost | 4 500
| |
| Since version | 0.23.5 | |
| Part configuration | part.cfg | |
| Maximum thrust | (1 atm) | 666.67 kN |
| (vacuum) | 750.00 kN | |
| Isp | (1 atm) | 160 s |
| (vacuum) | 180 s | |
| Fuel consumption | 56.65  /s
| |
| Thrust vectoring | No | |
| Burn time | (1 atm) | 0.5 s |
| (vacuum) | 0.5 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 | Yes | |
| Test by staging | Yes | |
| Manually testable | No | |
| Packed volume | None | |
| Solid fuel | 30
| |
