Vanguard (rocket)

Vanguard
Vanguard rocket on Pad LC-18A
FunctionSatellite launch vehicle
ManufacturerGlenn L. Martin Company
Country of originUnited States
Size
Height21.9 meters (72 ft)
Diameter1.14 meters (3 ft 9 in)
Mass10,050 kilograms (22,160 lb)
Stages3
Capacity
Payload to LEO
Mass11.3 kg (25 lb)
Launch history
StatusRetired
Launch sitesCape Canaveral, LC-18A
Total launches11
Success(es)3
Failure(s)8
First flight23 October 1957
(Vanguard 1: 17 March 1958)
Last flight18 September 1959
First stage – Vanguard
Height13.4 m (44 ft)
Diameter1.14 m (3 ft 9 in)
Empty mass811 kg (1,788 lb)
Gross mass8,090 kg (17,840 lb)
Powered by1 General Electric
GE X-405
Maximum thrust125,000 N (28,000 lbf)
Specific impulse248 s (2.43 km/s)
Burn time144 seconds
PropellantLOX / Kerosene (RP-1)
Second stage – Delta
Height5.8 m (19 ft)
Diameter0.8 m (2 ft 7 in)
Empty mass694 kg (1,530 lb)
Gross mass1,990 kg (4,390 lb)
Powered by1 Aerojet General AJ10-37
Maximum thrust32,600 N (7,300 lbf)
Specific impulse261 s (2.56 km/s)
Burn time120 seconds
PropellantUDMH / Nitric acid (IWFNA)
Third stage – Grand Central Rocket Company
or Allegany Ballistics Laboratory (last)
Height1.5 m (4 ft 11 in)
Diameter0.8 m (2 ft 7 in)
Empty mass31 kg (68 lb)
Gross mass194 kg (428 lb)
Powered by1
Maximum thrust10,400 N (2,300 lbf)
Specific impulse230 s (2.3 km/s)
Burn time30 seconds
PropellantSolid

The Vanguard rocket[1] was intended to be the first launch vehicle the United States would use to place a satellite into orbit. Instead, the Sputnik crisis caused by the surprise launch of Sputnik 1 led the U.S., after the failure of Vanguard TV-3, to quickly orbit the Explorer 1 satellite using a Juno I rocket, making Vanguard 1 the second successful U.S. orbital launch.

Vanguard rockets were used by Project Vanguard from 1957 to 1959. Of the eleven Vanguard rockets which the project attempted to launch, three successfully placed satellites into orbit. Vanguard rockets were an important part of the Space Race between the United States and the Soviet Union.

  1. ^ B. Klawans. (April 1960). "The Vanguard Satellite Launching Vehicle — An Engineering Summary. Martin Company Engineering Report No 11022" (PDF). Archived from the original (PDF) on 3 February 2006. PDF of an optical copy. Public Domain This article incorporates text from this source, which is in the public domain.

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