Difference between revisions of "Launch Escape System/Box"

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Revision as of 10:10, 30 April 2015

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
Launch Escape System
Part image
Launch escape system by
Kerbodyne

Radial size Small
Cost (total) 1 000.00 Funds
(dry) 982.00 Funds
Mass (total) 1.125 t
(dry) 0.900 t
Drag 0.2-0.3
Max. Temp. 2200 K
Impact Tolerance 15 m/s
Research Advanced landing.png Landing
Unlock cost 4 500 Funds
Since version 0.23.5
Part configuration part.cfg
Maximum thrust (1 atm) 592.60 kN
(vacuum) 666.67 kN
Isp (1 atm) 160 s
(vacuum) 180 s
Fuel consumption 50.36 Units of fuel/s
Thrust vectoring No
Burn time (1 atm) 0.5 s
(vacuum) 0.6 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