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

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

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supply 25% more thrust, and three <strong>of</strong> the boosters are<br />

equipped with thrust vec<strong>to</strong>r control for better maneuverability.<br />

A new 4-m-diameter payload fairing <strong>to</strong>ps the<br />

assembly. <strong>The</strong> first Delta III was launched in August<br />

1998 and, like the very first Delta, carried a real payload—the<br />

Hughes Galaxy-X communications satellite—<br />

rather than a test article. Unfortunately, it also suffered<br />

the same fate, as a directional control problem doomed<br />

the flight. <strong>The</strong> second Delta III launch, in May 1999,<br />

also failed due <strong>to</strong> a rupture in the thrust chamber <strong>of</strong> the<br />

RL10 engine. <strong>The</strong> third flight, on August 23, 2000, was<br />

successful but carried only a test payload.<br />

Although the Delta III has a backlog <strong>of</strong> about 20<br />

launches, its manufacturer, Boeing, already has plans<br />

Sample Delta Launch Vehicles<br />

<strong>to</strong> phase it out in favor <strong>of</strong> the Delta IV. This latest<br />

extension <strong>of</strong> the Delta dynasty, which uses a new liquid<br />

oxygen/liquid hydrogen common core booster powered<br />

by a single RS68 engine, is being developed under<br />

the Air Force EELV contract. Delta IV comes in five<br />

variants, ranging from the Delta IVM (medium), which<br />

will replace the Delta II, <strong>to</strong> the <strong>to</strong>p-<strong>of</strong>-the-line Delta IV<br />

“heavy,” which combines three common core boosters<br />

with a large Delta III-type LOX/LH2 second stage and<br />

a new 5-m fairing <strong>to</strong> place up <strong>to</strong> 13,130 kg in<strong>to</strong> GTO.<br />

Together, the Delta IV variants are capable <strong>of</strong> replacing<br />

not only the current Delta IIs and IIIs but also the<br />

more powerful Titan IV. <strong>The</strong> maiden flight <strong>of</strong> the Delta<br />

IV was scheduled for November 2002. (See table.)<br />

Diameter First-Stage Payload (kg)<br />

Length (m) Max. (m) Thrust (N)* LEO GTO<br />

Original Delta 27.4 2.4 670,000 270 45<br />

Delta A 27.4 2.4 760,000 320 68<br />

Delta B 28.3 2.4 760,000 375 68<br />

Delta C 28.3 2.4 760,000 410 80<br />

Delta D 28.3 2.4 1,725,000 580 105<br />

Delta E 29.2 2.4 1,644,000 725 150<br />

Delta L 32.4 2.4 1,725,000 n/a —<br />

Delta M-6 32.4 2.4 2,421,000 1,300 450<br />

Delta 904 32.4 2.4 3,236,000 — 640<br />

Delta 1914 32.4 2.4 3,362,000 — 680<br />

Delta 2914<br />

Delta 3000<br />

32.4 2.4 3,362,000 2,000 720<br />

Original 3000 32.4 2.4 4,321,000 — 950<br />

With PAM-D 32.4 2.4 4,632,000 — 1,270<br />

Delta 4914 39.0 2.4 5,337,000 3,400 1,360<br />

Delta II 6925<br />

Delta II 7000<br />

39.0 2.4 5,339,000 3,980 1,450<br />

7320 40.5 3.0 2,387,000 2,730 900<br />

7925H-10L 40.5 3.0 5,382,000 5,090 1,830<br />

Delta III<br />

Delta IV<br />

41.0 4.0 6,540,000 8,290 3,810<br />

Medium 63.0 5.0 2,891,000 6,760 3,900<br />

Medium-plus (4,2) 63.0 4.0 4,103,000 9,070 5,850<br />

Medium-plus (5,2) 69.0 5.0 4,103,000 7,850 4,640<br />

Medium-plus (5,4) 69.0 5.0 5,315,000 10,300 6,570<br />

Heavy 70.7 5.0 8,673,000 20,500 13,130<br />

*Includes any ground-lit or air-lit strap-ons.<br />

105

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