Search results

Jump to: navigation, search
  • ...we will never 'catch up' to the event horizon. Since this singularity is artificial, it decays almost instantaneously without constant graviton embardment. We ...YSE drive's movement, there is significant jerk during the launch and stop procedures. The drive can achieve a target velocity within a matter of seconds, at si
    8 KB (1,300 words) - 13:19, 9 December 2016
  • '''These procedures are no longer applicable to Spacesim''' All docking procedures are shuttle operation procedures except:
    621 B (95 words) - 11:45, 30 March 2010
  • ==== General Procedures==== ...the astronauts. If in space, deactivate the [[3DMI]] to remove artificial gravity. If the astronauts are dead, follow P4.4.4.
    2 KB (293 words) - 14:36, 25 October 2014
  • ...re monitored on the [[Power Grid]] software according to the [[Engineering Procedures]]. [[Image:ENG software.jpg|thumb|right|500px|The [[Power Grid]] software: ;[[Artificial Gravity]] (A GRAV): Inertial dampening system to reduce acceleration strain on Habi
    7 KB (1,049 words) - 18:51, 10 June 2010
  • ...rg/OCESS%20procedures.pdf procedures]. All the information on the outdated procedures is also included in hard copy in [[Non-Computer Named Objects#Other items|T ==OCESS Procedures Manual==
    3 KB (277 words) - 19:40, 28 November 2014
  • 10:52 PM 03/01/2011: Artificial gravity engaged momentarily in order to stretch and retrieve personal effects. 3:23 PM 03/02/2011: Beginning gravity assist with Mars
    69 KB (10,437 words) - 18:56, 27 November 2015
  • ==Procedures== ...{{procs|Engineering}} chapter of the [[Procedures Table of Contents|OCESS Procedures Manual]] including:
    1 KB (161 words) - 16:39, 26 April 2010

View (previous 50 | next 50) (20 | 50 | 100 | 250 | 500)