Control System Orbit Attitude Maneuver System (OAMS) Propulsion. Mission: GT-5. NASA Manned Spacecraft Center, 11 May 1965. Single sheet, 11 by 17 inches. Issued to Gordon Cooper and features control valves with fuel/oxidizer lines plus electrical line schematics of the Gemini spacecraft OAMS rocket propulsion system. WITH: Spacecraft 5 Estimated OAMS Propellant Depletion with Permeation Effects Included. Single sheet, 11 by 17 inches. Plots the percentage of usable propellant quantity (338 total pounds) verses available helium source pressure in PSIA relative to source temperature.
Control System Orbit Attitude Maneuver System (OAMS) Propulsion. Mission: GT-5. NASA Manned Spacecraft Center, 11 May 1965. Single sheet, 11 by 17 inches. Issued to Gordon Cooper and features control valves with fuel/oxidizer lines plus electrical line schematics of the Gemini spacecraft OAMS rocket propulsion system. WITH: Spacecraft 5 Estimated OAMS Propellant Depletion with Permeation Effects Included. Single sheet, 11 by 17 inches. Plots the percentage of usable propellant quantity (338 total pounds) verses available helium source pressure in PSIA relative to source temperature.
.jpg "Source: Christie's")
Try LotSearch and its premium features for 7 days - without any costs!
Be notified automatically about new items in upcoming auctions.
Create an alert
.jpg "Source: Christie's")
.jpg "Source: Christie's")
