Difference between revisions of "Launch Escape System/Box"
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m (+mod parameter to allow the new NASA mission configurations;) |
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
− | |file= | + | |file=Launch_Escape_System.png |
|role=Launch escape system | |role=Launch escape system | ||
+ | |size=s | ||
|manufacturer=KD | |manufacturer=KD | ||
− | + | |costs=1000 | |
− | |costs= | + | |mass=0.9 |
− | |mass= | + | |sf=30.000 |
− | |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 | ||
+ | |fuel=30.0 | ||
+ | |isp-atm=160 | ||
+ | |isp-vac=180 | ||
|thrust=750 | |thrust=750 | ||
− | | | + | }} |
− | | | + | {{Infobox/Part/test subject |
− | | | + | |environments=5 |
+ | |event=False | ||
+ | |staging=True | ||
}} | }} | ||
}} | }} |
Latest revision as of 18:26, 17 March 2017
Launch Escape System | ||
Launch escape system by Kerbodyne | ||
Radial size | Small | |
Cost | (total) | 1 000.00 |
(dry) | 982.00 | |
Mass | (total) | 1.13 t |
(dry) | 0.90 t | |
Drag | 0.2-0.3 | |
Max. Temp. | 2700 K | |
Volume | ? | |
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 | |
Fuel | 30.0 | |
Burn time | (1 atm) | 0.5 s |
(vacuum) | 0.5 s | |
Testing Environments | ||
On the surface | Yes | |
In the ocean | No | |
On the launchpad | Yes | |
In the atmosphere | No | |
Sub orbital | No | |
In an orbit | No | |
On an escape | No | |
Docked | No | |
Test by staging | Yes | |
Manually testable | No |