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The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity

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104<br />

(GEMs) for improved performance. It bears little<br />

resemblance <strong>to</strong> the original Thor-Delta. With a height<br />

<strong>of</strong> 41 m, the Delta 7925 stands over 10 m taller than its<br />

ances<strong>to</strong>r and has a GTO payload capacity <strong>of</strong> about<br />

1,870 kg—more than 40 times that <strong>of</strong> the Thor-Delta.<br />

Delta III and IV<br />

Almost four decades <strong>of</strong> continual development have<br />

increased the Delta’s payload capacity by steady incre-<br />

Delta A Delta II launches an<br />

Iridium communications satellite<br />

from Vandenberg Air Force<br />

Base. Lockheed Martin<br />

ments. <strong>The</strong> Delta III, however, represents a sudden leap<br />

in capacity <strong>to</strong> over twice that <strong>of</strong> the largest Delta II. A<br />

major part <strong>of</strong> this improvement is due <strong>to</strong> the Delta III’s<br />

second stage, powered by a Pratt & Whitney RL10B<br />

engine derived from the RL10 that has been the basis<br />

<strong>of</strong> the Centaur for over 30 years. Burning liquid hydrogen<br />

and liquid oxygen, the RL10B has a world-record<br />

specific impulse rating (an efficiency measure) <strong>of</strong> 462<br />

seconds and represents the first use <strong>of</strong> a high-energy<br />

cryogenic engine in a Delta. Additionally, new SRBs

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