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

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<strong>Explor<strong>in</strong>g</strong> <strong>the</strong> <strong>Unknown</strong> 89<br />

V. Instrumentation<br />

Medical <strong>in</strong>strumentation required to evaluate <strong>the</strong> pilot’s reaction to space<br />

flight will be <strong>in</strong>corporated <strong>in</strong> <strong>the</strong> capsule. In addition, <strong>in</strong>strumentation will be<br />

provided to measure and monitor <strong>the</strong> <strong>in</strong>ternal and external cab<strong>in</strong> environment<br />

and to make scientific observations. <strong>The</strong>se data will be recorded <strong>in</strong> flight and/or<br />

telemetered to ground recorders.<br />

VI. Communication<br />

Provisions will be made for adequate two-way communications between <strong>the</strong><br />

pilot and ground stations. [3]<br />

VII. Ground Support<br />

<strong>The</strong> successful completion of <strong>the</strong> manned satellite program will require considerable<br />

ground support, such as pre-launch support and an elaborate recovery network.<br />

VIII. Test Program<br />

An extensive test program will be required to implement this project. <strong>The</strong><br />

test program will <strong>in</strong>clude ground test<strong>in</strong>g, development and qualification flight<br />

test<strong>in</strong>g, and pilot tra<strong>in</strong><strong>in</strong>g.<br />

Document I-13<br />

Document Title: NASA, “Prelim<strong>in</strong>ary Specifications for Manned Satellite<br />

Capsule,” October 1958.<br />

Source: Folder 18674, NASA Historical Reference Collection, NASA History<br />

Division, NASA Headquarters, Wash<strong>in</strong>gton DC.<br />

Most of <strong>the</strong> design work for what became <strong>the</strong> Mercury spacecraft took place under <strong>the</strong> auspices<br />

of, and <strong>in</strong> many cases directly by, Max Faget. This document, written by Faget and his<br />

research team, established very detailed specifications for <strong>the</strong> Mercury spacecraft for <strong>the</strong> use<br />

of <strong>in</strong>dustry, necessary for <strong>the</strong>ir proposals to build <strong>the</strong> hardware. <strong>The</strong>se specifications outl<strong>in</strong>ed<br />

<strong>the</strong> program and suggested methods of analysis and construction. Faget specifically asked for<br />

<strong>the</strong> construction of a simple, nonlift<strong>in</strong>g vehicle that could follow a ballistic path <strong>in</strong> reenter<strong>in</strong>g<br />

<strong>the</strong> atmosphere without experienc<strong>in</strong>g heat<strong>in</strong>g rates or accelerations that would be dangerous<br />

to an astronaut. He also called for modest pitch, yaw, and attitude control, as well as<br />

a retrorocket pack to br<strong>in</strong>g <strong>the</strong> capsule down from orbital velocity. F<strong>in</strong>ally, this document<br />

established <strong>the</strong> limits of size, shape, weight, and tolerances of <strong>the</strong> Mercury spacecraft. This<br />

set of specifications became <strong>the</strong> basis for <strong>the</strong> capsule’s construction by <strong>the</strong> McDonnell Aircraft<br />

Company based <strong>in</strong> St. Louis, Missouri.<br />

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION<br />

PRELIMINARY SPECIFICATIONS<br />

FOR<br />

MANNED SATELLITE CAPSULE

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