Editing Escape Pods

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The ASRV measures 3x3x3 m and its shape is characterized as a truncated cube. The total mass is 1.35 metric tones. It's internal space frame is a standard beam and stringer arrangement, constructed from gamma-welded titanium and frumium monocarbonite. The frame is skinned with single crystal micro-filleted tritanium with umbilical passthroughs, conformal emitters, and sensors doped with hafnium cobarate for passive thermal control during atmosphere entry.
The ASRV measures 3x3x3 m and its shape is characterized as a truncated cube. The total mass is 1.35 metric tones. It's internal space frame is a standard beam and stringer arrangement, constructed from gamma-welded titanium and frumium monocarbonite. The frame is skinned with single crystal micro-filleted tritanium with umbilical passthroughs, conformal emitters, and sensors doped with hafnium cobarate for passive thermal control during atmosphere entry.


Propulsion is available from three different systems. The ejector initiator is a single pulse, buffered microfusion device that propels the lifeboat through the launch channel. Power is tapped from the fusion reaction to start the lifeboats inertial dampening field and gravity generator.
Propulsion is available from three different systems. The ejector initiator is a single pulse, buffered microfusion device that propels the lifeboat through the launch channel. Power is tapped from the fusion reaction to start the lifeboats inertial dampening field and gravity generator.


The main impulse engine, a low-power microfusion system for all primary spacecraft maneuvering, is rated at a maximum thrust of 9500 Newtons and is fed from a 75kg deuterium fuel supply. The reaction control system provides precise attitude control in space, and maneuvering during planetary landing.
The main impulse engine, a low-power microfusion system for all primary spacecraft maneuvering, is rated at a maximum thrust of 9500 Newtons and is fed from a 75kg deuterium fuel supply. The reaction control system provides precise attitude control in space, and maneuvering during planetary landing.
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