Editing Shuttle-A
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| Latest revision | Your text | ||
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|rcs_engine=5 kN | |rcs_engine=5 kN | ||
|rcs_engine_isp=30 kN·s/kg | |rcs_engine_isp=30 kN·s/kg | ||
| − | |max_deltav= | + | |max_deltav=54.9 km/s |
|max_accel=23.0 m/s<sup>2</sup> | |max_accel=23.0 m/s<sup>2</sup> | ||
|docking_port_template=1DockingPort | |docking_port_template=1DockingPort | ||
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the Moon, Mars, and potentially moons in the outer solar system. In its current | the Moon, Mars, and potentially moons in the outer solar system. In its current | ||
configuration it is also capable of achieving orbit from Earth's surface, but this requires a | configuration it is also capable of achieving orbit from Earth's surface, but this requires a | ||
| − | precise ascent profile | + | precise ascent profile. |
The engine layout consists of a set of two main engines, two hover engines, and two engines | The engine layout consists of a set of two main engines, two hover engines, and two engines | ||
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The Shuttle-A contains a docking port and airlock below the habitat module which is protected | The Shuttle-A contains a docking port and airlock below the habitat module which is protected | ||
by a hatch during atmospheric flight. | by a hatch during atmospheric flight. | ||
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