Editing Shuttle-A

{{Infobox Vessel|name=Shuttle-A
|pic1_file=ShA-Scrshot1.jpg
|pic1_text=Shuttle-A
|full_name=Shuttle-A
|role=Low gravity/low pressure cargo hauler
|crew=2
|passengers=none
|first_flight_date=date unknown
|service_date=date unknown
|manufacturer=unknown
|length=35.0 m 
|height=6.98 m
|width=15.4 m
|empty_mass=22,000 kg
|fuel_mass=16,000 kg
|rcs_fuel_mass=700 kg
|max_takeoff_mass=38,700 kg
|inertia_pmi=86.6/89.8/5.5 m<sup>2</sup>
|main_engine_template=Engine
|main_engine=2 x 193.52 kN
|main_engine_isp=30 kN·s/kg
|retro_engine_template=N/A
|hover_engine_template=Engine
|hover_engine=2 x 135.45 kN
|hover_engine_isp=30 kN·s/kg
|aux_engine_template=Engine
|aux_engine=2 x 60 kN
|aux_engine_isp=30 kN·s/kg
|rcs_engine_template=Engine
|rcs_engine=5 kN
|rcs_engine_isp=30 kN·s/kg
|max_deltav=16.4 km/s
|max_accel=23.0 m/s<sup>2</sup>
|docking_port_template=1DockingPort
|docking_port_1=front

}}

The Shuttle-A is a cargo {{noun}} designed for a low {{noun}}/low {{noun}} operational
{{noun}}. Its primary {{noun}} of deployment is for transport duty between [[LEO]],
the {{noun}}, {{noun}}, and potentially {{noun plural}} in the outer solar system. In its current
{{noun}} it is also capable of achieving orbit from Earth's surface, but this requires a
precise ascent {{noun}}.

The engine layout consists of a set of two main {{noun plural}}, two hover {{noun plural}}, and two {{noun plural}} in central side {{noun plural}} which can be rotated for hover or retro duty. There are two different propellant systems for main and RCS {{noun plural}}.

The Shuttle-A contains a docking {{noun}} and {{noun}} below the habitat {{noun}} which is protected
by a {{noun}} during atmospheric flight.

[[Category:Vessels of Orbiter]]
@@ Line 37: / Line 37: @@
 }}
-The Shuttle-A is a cargo vessel designed for a low gravity/low pressure operational
+The Shuttle-A is a cargo {{noun}} designed for a low {{noun}}/low {{noun}} operational
-environment. Its primary area of deployment is for transport duty between [[LEO]],
+{{noun}}. Its primary {{noun}} of deployment is for transport duty between [[LEO]],
-the Moon, Mars, and potentially moons in the outer solar system. In its current
+the {{noun}}, {{noun}}, and potentially {{noun plural}} in the outer solar system. In its current
-configuration it is also capable of achieving orbit from Earth's surface, but this requires a
+{{noun}} it is also capable of achieving orbit from Earth's surface, but this requires a
-precise ascent profile. Due to its design it is not aerodynamic nor does it provide any lift such as other spacecraft such as the [[Delta-glider]]. This means maneuvers in atmosphere are very difficult.
+precise ascent {{noun}}.
-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 {{noun plural}}, two hover {{noun plural}}, and two {{noun plural}} in central side {{noun plural}} which can be rotated for hover or retro duty. There are two different propellant systems for main and RCS {{noun plural}}.
-in central side pods which can be rotated for hover or retro duty. There are two different
-propellant systems for main and RCS engines.
-The Shuttle-A contains a docking port and airlock below the habitat module which is protected
+The Shuttle-A contains a docking {{noun}} and {{noun}} below the habitat {{noun}} which is protected
-by a hatch during atmospheric flight.
+by a {{noun}} during atmospheric flight.
-<gallery>
-ShuttleAOrbiter2001.jpg|<center>Shuttle-A in Orbiter 2001</center>
-ShuttleA-orbiter2002p3.jpg|<center>Shuttle-A in Orbiter 2002P3</center>
-ShuttleA-Orbiter2003P2.jpg|<center>Shuttle-A in Orbiter 2003P2</center>
-ShuttleA-Orbiter2005P1.jpg|<center>Shuttle-A in Orbiter 2005P1</center>
-ShuttleA-Orbiter2006P1.jpg|<center>Shuttle-A in Orbiter 2006P1</center>
-ShuttleA-Orbiter2010P1-Orbiter2010P1.jpg|<center>Shuttle-A in Orbiter 2010P1</center>
-</gallery>
-[[Category: Articles]]
 [[Category:Vessels of Orbiter]]