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Exploring the Unknown: Selected Documents in ... - The Black Vault

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272<br />

First Steps <strong>in</strong>to Space: Projects Mercury and Gem<strong>in</strong>i<br />

MSC standard meteoroid environment, <strong>the</strong> follow<strong>in</strong>g weight of soft<br />

goods padd<strong>in</strong>g will be required <strong>in</strong> a protective garment:<br />

a. Phase One (10 m<strong>in</strong>utes) - 2 lb.<br />

b. Phase Two (30 m<strong>in</strong>utes) – 3.5 lb.<br />

c. Phase Three (1 hour) – 4.75 lb.<br />

2. Development of a meteoroid protective garment is to be carried out<br />

by CSD.<br />

E. Te<strong>the</strong>r.<br />

1. A te<strong>the</strong>r <strong>in</strong>corporat<strong>in</strong>g a safety l<strong>in</strong>e and communications leads is<br />

be<strong>in</strong>g developed by CSD. Initial plann<strong>in</strong>g has been based on no<br />

biomedical <strong>in</strong>strumentation dur<strong>in</strong>g <strong>the</strong> extravehicular operation.<br />

More recently CSD and Medical Operations have [6] specified<br />

m<strong>in</strong>imum desired parameters to be monitored. Provisions for<br />

monitor<strong>in</strong>g <strong>the</strong>se parameters will be <strong>in</strong>corporated <strong>in</strong> <strong>the</strong> te<strong>the</strong>r, if<br />

possible. <strong>The</strong> length of <strong>the</strong> te<strong>the</strong>r is to be sufficient to allow <strong>in</strong>gress<br />

to <strong>the</strong> equipment adapter section.<br />

F. Maneuver<strong>in</strong>g Unit.<br />

1. <strong>The</strong> Air Force has proposed an extravehicular unit (MMU) for use<br />

on later Gem<strong>in</strong>i missions under Gem<strong>in</strong>i/DOD Experiment 14C. If<br />

this experiment is approved, it is anticipated that <strong>the</strong> MMU would<br />

be used <strong>in</strong> <strong>the</strong> latter part of Phase Two and <strong>in</strong> Phase Three. <strong>The</strong><br />

MMU would conta<strong>in</strong> propulsion, control, communications, and life<br />

support systems. It would be furnished by <strong>the</strong> Air Force under an<br />

<strong>in</strong>dependent contract.<br />

V. SPACECRAFT MODIFICATIONS<br />

A. Spacecraft modifications will be <strong>in</strong>corporated to enable <strong>the</strong><br />

astronaut to move about <strong>the</strong> exterior of <strong>the</strong> spacecraft and <strong>in</strong>to <strong>the</strong><br />

equipment adapter. <strong>The</strong>se modifications are as follows:<br />

1. Exterior handholds spaced approximately two feet apart from <strong>the</strong><br />

cockpit to <strong>the</strong> adapter section <strong>in</strong>terior. <strong>The</strong> handle configuration<br />

will be based on configuration studies by CSD as well as aerodynamic<br />

considerations.<br />

2. Protective cover for <strong>the</strong> rough edge at <strong>the</strong> aft end of <strong>the</strong> adapter<br />

section. <strong>The</strong> astronaut must be able to proceed past this rough edge<br />

without <strong>the</strong> hazard of damage to <strong>the</strong> pressure suit or <strong>the</strong> te<strong>the</strong>r.<br />

Document I-54<br />

Document Title: Edward Z. Gray, Director, Advanced Manned Missions Program,<br />

Office of Manned Space Flight, NASA, to Director, Gem<strong>in</strong>i Program, NASA,<br />

“Gem<strong>in</strong>i Lunar Mission Studies,” 30 April 1964.

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