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

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184<br />

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

to <strong>the</strong> astronaut were to occur) could result <strong>in</strong> an unnecessary abort. This aga<strong>in</strong><br />

results <strong>in</strong> a reduction, but not necessarily below acceptable limits, of astronaut<br />

survivability.<br />

3. Redundant or Backup Systems<br />

Dur<strong>in</strong>g <strong>the</strong> presentations a great deal of stress was placed on <strong>the</strong> many<br />

redundant features of <strong>the</strong> entire system. <strong>The</strong> basic need for alternate ways to<br />

br<strong>in</strong>g <strong>the</strong> astronaut to safety <strong>in</strong> case of system failure centers around <strong>the</strong> desire<br />

to provide much more reliable over-all operation than can be assured from <strong>the</strong><br />

presently available reliability of ei<strong>the</strong>r <strong>the</strong> Atlas or Redstone boosters. In addition,<br />

many newly designed subsystems are <strong>in</strong>volved, and <strong>the</strong>re is no way to guarantee an<br />

acceptable reliability without an <strong>in</strong>ord<strong>in</strong>ate amount of test<strong>in</strong>g, unless <strong>the</strong> backup<br />

or redundant system philosophy is adopted.<br />

<strong>The</strong> follow<strong>in</strong>g chart illustrates <strong>the</strong> multiple possibilities which are available<br />

to br<strong>in</strong>g <strong>the</strong> astronaut to safety <strong>in</strong> case of a subsystem failure. [9]<br />

Critical Functions or Events<br />

Accelerate to altitude<br />

Initiation of abort<br />

Release of escape rocket<br />

tower, and Separation from<br />

booster bolts.<br />

Oxygen environment for<br />

astronaut<br />

Monitor<strong>in</strong>g astronaut’s<br />

condition<br />

Attitude control of Capsule<br />

Retro-fire<br />

Land<strong>in</strong>g<br />

Recovery<br />

Redundant Modes of Operation or Actuation<br />

Normal booster operation – Abort by use of<br />

escape rockets<br />

Radio command from Control Center or<br />

Blockhouse; direct actuation by astronaut; radio<br />

command by range safety; abort sens<strong>in</strong>g and<br />

implementation system.<br />

Electrical explod<strong>in</strong>g bolts; alternate electrically<br />

explod<strong>in</strong>g bolts; direct activated explod<strong>in</strong>g<br />

Capsule pressurization; space suit with separate<br />

oxygen system; emergency oxygen supply<br />

Telemetry of biomedical <strong>in</strong>struments; UHF<br />

voice l<strong>in</strong>k; alternate UHF voice l<strong>in</strong>k; HF voice<br />

l<strong>in</strong>k; manual key on telemetry l<strong>in</strong>k.<br />

Automatic stabilization control system with dual<br />

sets of jets; manual control system with separate<br />

set of jets; switch-over between <strong>the</strong> two systems.<br />

Three rockets when two are needed; two fir<strong>in</strong>g<br />

mechanisms and two power supplies.<br />

Normal parachutes descent of capsule;<br />

emergency chute for <strong>the</strong> capsule, and <strong>in</strong><br />

Redstone flight a personal chute for astronaut<br />

egress from capsule top hatch; and emergency<br />

side hatch<br />

Helicopter pickup <strong>in</strong> water plus numerous<br />

ground and sea pickup arrangements. [10]

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