David Meerman Scott

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Flown Apollo 9 Command Module flown cue card

  This oddly shaped cue card fit snugly into a particular spot on the command module control panel. The cue card provides quick instructions for problems faced by the crew. I really like this cue card because some of the issues it deals with – such as Oxygen, CO2, Glycol, and Cyro – uses instrument […]

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Apollo 13 Lunar Module TD+2 Star Chart used in training

  This 8-3/4″ diameter star chart consists of a black star disc below and a semitransparent rotating disc. The rings on the outer disc signify what stars would be seen through the LM Optical Telescope at certain times during the stay on the moon. Star charts like this were used on every lunar landing mission

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Apollo 13 CSM Launch Checklist used in training

  This checklist containing more than 100 pages on 8 by 6 inch card stock was the personal training copy of Apollo 13 lunar module pilot Fred Haise. This manual lists the events that occurred during the Saturn V launch and has specific steps to be carried out by the flight crew. Sections cover boost

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Apollo 13 flown launch abort cue card

This cue card was from the personal collection of Fred W. Haise, Apollo 13 Lunar Module Pilot. The information that Haise supplied about the card reads: “This cue card was carried around the moon on the flight of Apollo 13 during April 11 to 17, 1971. This card was positioned on the instrument panel with

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Apollo Spacecraft News Reference for Lunar Module and Command Module

These Apollo News Reference Manuals were used by journalists who covered the Apollo program. It took me four years to acquire a pair as these manuals have become highly sought after. The pair include almost 500 pages of in depth detail about the Apollo spacecraft in the words of the contractors who built them. Chapters

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Apollo Service Module RCS Helium Pressurization Solenoid Valve

Apollo Service Module RCS Helium Pressurization Solenoid Valve Helium is supplied to the Reaction Control System propellant with the helium pressure used drive the propellant out of the bladders at the proper feed rate to the R-4D reaction control engines in the quads. The helium isolation valves between the helium tank and pressure regulators contain

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Apollo Saturn S-II (Second Stage) liquid hydrogen vent and relief valve

Apollo Saturn S-II (Second Stage) Liquid Hydrogen (LH2) dual function tank Vent and Relief Valve was manufactured by Wallace O. Leonard Inc. under subcontract to North American Aviation (prime for the S-II). The valve was produced in 1966. The LH2 Vent-Relief valve, used as part of the single Rocketdyne J-2 engine system which powered the

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