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

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68<br />

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

and maximum stagnation temperature of 3500 O F; maximum deceleration - 8<br />

g’s. Although it could be accomplished one and one half years sooner, he dismissed<br />

<strong>the</strong> sphere as hav<strong>in</strong>g no growth potential. Bell’s proposal <strong>the</strong>refore h<strong>in</strong>ged<br />

strongly on <strong>the</strong>ir ROBO concept. <strong>The</strong> glide vehicle is outl<strong>in</strong>ed <strong>in</strong> <strong>the</strong> follow<strong>in</strong>g.<br />

Pert<strong>in</strong>ent Features<br />

Vehicle: Glider. [Diagram with Coolant, Control Console, Equipment]<br />

Weight: 18,800 pounds.<br />

Boosters. Several assembled configurations were discussed. <strong>The</strong> one favored<br />

was a three-stage clustered configuration with three Titans, one Titan, One F 2<br />

-<br />

NH 3<br />

rocket, as diagrammed below:<br />

Initial gross weight would be 747,000 Pounds; 1 = 521,300 pounds, 2<br />

= 175,300 pounds, 3 = 31,300 pounds, airplane - 18,800 pounds, research<br />

equipment 1500 pounds. Total propellants would be 659,500 pounds. Maximum<br />

acceleration - 4 g’s.<br />

[22]<br />

Time and altitude: 127 m<strong>in</strong>utes duration. Boost for seven m<strong>in</strong>utes. Altitude at<br />

end of boost - 260,000 feet. Follow maximum L/D (Breguet) path.<br />

Recovery and land<strong>in</strong>g: Conventional man-controlled glider land<strong>in</strong>g.<br />

Navigation: Self-conta<strong>in</strong>ed.<br />

Schedule: Five years. Flight <strong>in</strong> 1963.

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