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

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462 Vega 1 and 2<br />

seven operational launches (called SLV for “space<br />

launch vehicle”) were successful—a failure rate unsurpassed<br />

by any other American launch vehicle.<br />

Adapted from the U.S. Navy’s Viking and Aerobee<br />

research rockets, Vanguard was designed <strong>to</strong> fulfill the<br />

Eisenhower Administration’s goal <strong>of</strong> placing a small<br />

scientific satellite in orbit during the International<br />

Geophysical Year (IGY). Its development stemmed<br />

from a 1955 study <strong>to</strong> determine which vehicle would<br />

be most suitable for launching the first American<br />

satellite. Among the proposals rejected were Project<br />

Orbiter, a Reds<strong>to</strong>ne-based plan put forward by the<br />

Army Ballistic Missile Agency (ABMA). At the height<br />

<strong>of</strong> the Cold War, Eisenhower was sensitive about<br />

allowing the military <strong>to</strong> launch the first American<br />

satellite. Although the Vanguard program was based<br />

on the Navy Viking, it was proposed under civilian<br />

management and so was selected ahead <strong>of</strong> its rivals. At<br />

least six Vanguard rockets had been scheduled for test<br />

launches prior <strong>to</strong> what would have been the first<br />

American attempt <strong>to</strong> l<strong>of</strong>t a satellite. Since the IGY ran<br />

from July 1, 1957, through December 31, 1958, it was<br />

thought there would be plenty <strong>of</strong> time for the Vanguard<br />

<strong>to</strong> prove itself before attempting <strong>to</strong> reach orbit.<br />

However, technical problems quickly surfaced, and<br />

the first test launch was delayed until December 8,<br />

1956. A second test <strong>to</strong>ok place on May 1, 1957, but<br />

before there could be a third, the Soviet Union shook<br />

the world with their launch <strong>of</strong> Sputnik 1 on Oc<strong>to</strong>ber<br />

4, 1957. To counter this unexpected Soviet coup, and<br />

that <strong>of</strong> Sputnik 2 in November 1957, a bold decision<br />

was made <strong>to</strong> go for a satellite launch aboard the next<br />

available Vanguard (TV-3). However, TV-3 exploded<br />

on its launch pad before the eyes <strong>of</strong> the world on<br />

December 6, 1957. This public debacle cleared the<br />

way for ABMA <strong>to</strong> attempt, and successfully achieve,<br />

the launch <strong>of</strong> America’s first satellite, Explorer 1, on<br />

January 31, 1958. Despite the highly publicized Vanguard<br />

failure, the program didn’t immediately end. A<br />

second, but less spectacular, Vanguard failure<br />

occurred during a follow-up satellite launch attempt<br />

on February 5, 1958. But then came success. <strong>The</strong> next<br />

Vanguard rocket carried the Vanguard 1 satellite in<strong>to</strong><br />

orbit on March 17, 1958. <strong>The</strong> next four attempts <strong>to</strong><br />

reach orbit failed, but Vanguard 2 was successfully<br />

launched on February 17, 1959. After two more failures,<br />

the last launch <strong>of</strong> a Vanguard rocket ended in triumph,<br />

placing Vanguard 3 in orbit on September 18,<br />

1959. Though the program was then quietly wound<br />

up, Vanguard technology was successfully applied <strong>to</strong><br />

other programs. <strong>The</strong> Vanguard’s upper stages formed<br />

the basis for upper stage configurations used on Atlas-<br />

Able, Thor-Able, and Scout rockets, and even found<br />

their way in<strong>to</strong> the <strong>Apollo</strong> program. A modified Vanguard<br />

upper stage served as the second stage <strong>of</strong> the<br />

Atlas-Antares, a rocket used <strong>to</strong> test various <strong>Apollo</strong><br />

reentry vehicle designs. (See table, “Vanguard Launch<br />

Vehicle Specifications.”)<br />

Length: 21.9 m<br />

Diameter: 1.1 m<br />

Vanguard Launch Vehicle Specifications<br />

First Stage Second Stage Third Stage<br />

Manufacturer GE (Viking) Aerojet Altair<br />

Fuel LOX/kerosene IWFNA/UDMH Solid<br />

Thrust (N) 124,000 33,000 13,800<br />

Vega Missions<br />

Spacecraft Launch Date Notes<br />

Vega 1 Dec. 15, 1984 Ejected Venus lander Jun. 10, 1985; Halley flyby on Mar. 6, 1986<br />

Vega 2 Dec. 21, 1984 Ejected Venus lander Jun. 14, 1985; Halley flyby on Mar. 9, 1986

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