Explorer S-1 (satellite)

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Explorer S-1
Juno II AM-16 (3).jpg
The Juno II launch vehicle carrying Explorer S-1 destroyed by the Range Safety Officer 5.5 seconds after liftoff.
NamesExplorer S-1
Explorer 7X
NASA S-1
Mission type Earth science
Operator NASA
COSPAR ID EXP-7X
Mission durationFailed to orbit
Spacecraft properties
SpacecraftExplorer S-1
Spacecraft typeScience Explorer
Bus S-1
Manufacturer Jet Propulsion Laboratory
Launch mass41.5 kg (91 lb)
Dimensions76 × 76 cm (30 × 30 in)
Start of mission
Launch date16 July 1959, 17:37:03 GMT
Rocket Juno II (AM-16)
Launch site Cape Canaveral, LC-5
Contractor Army Ballistic Missile Agency
End of mission
DestroyedFailed to orbit
Orbital parameters
Reference system Geocentric orbit (planned)
Regime Low Earth orbit
Perigee altitude 416 km (258 mi)
Apogee altitude 2,286 km (1,420 mi)
Inclination 49.9°
Period 112.7 minutes
Instruments
Ground Based Ionospheric
Heavy Primary Cosmic Rays
Micrometeorite
Solar X-Ray and Lyman-Alpha Radiation
Thermal Radiation
Trapped Radiation and Solar Protons
Explorer program
 

Explorer S-1, also known as NASA S-1 or Explorer 7X, [1] was a NASA Earth science satellite equipped with a suite of scientific instruments to study the environment around the Earth. The spacecraft and its Juno II launch vehicle were destroyed five seconds after launch on 16 July 1959, in a spectacular launch failure caused by complications with the launch vehicle's power supply. A relaunch of the mission in October 1959, Explorer 7 (S-1A), was successful.

Contents

Mission

The mission was planned to be the sixth flight of the Explorer program, designated NASA S-1 and Explorer 7X retrospectively. [2] The objectives of the mission were to measure the Earth's radiation balance, and the abundance of Lyman-alpha X-rays and cosmic rays, including heavy primary cosmic rays. [2] The spacecraft was also designed as a test bed for satellite capabilities, being equipped with instruments to measure the spacecraft's temperature, micrometeorite impacts, and the erosion of solar cells exposed to the vacuum of space. [2] The spin-stabilized spacecraft was 76 × 76 cm (30 × 30 in) in size, and had a launch mass of 41.5 kg (91 lb). [2] [3] The spacecraft's power was drawn from a bank of fifteen nickel–cadmium batteries recharged by 3,000 solar cells mounted on the exterior of the spacecraft. [3]

Launch

The spacecraft was mounted atop a Juno II launch vehicle with the serial AM-16. [4] It was launched on 16 July 1959, at 16:37:03 GMT, from Cape Canaveral Launch Complex 5 (LC-5). [5] Immediately after liftoff, a short circuit of the launch vehicle's guidance system caused the Rocketdyne S-3D engines to gimbal, tilting the rocket sharply to the west before almost flipping upside down. [3] [6] Five-and-a-half seconds after launch, the Range Safety Officer destroyed the launch vehicle. The launch vehicle's payload impacted the ground 76 m (249 ft) northwest of the launch site, resulting in a massive fireball. [3] [6]

Aftermath

In an investigation conducted after the launch failure, it was found that the short circuit occurred between two diodes in the launch vehicle's power supply inverter voltage regulator, cutting off power to the guidance system and causing a full gimbal. [6] Circuit board designs for the Juno II, and similar launch vehicles, subsequently used conformal coating to reduce the chances for a recurrence. [6] The launch, described by commentators as "infamous" and "one of the most spectacular failures ever seen at [Cape Canaveral]", [3] [6] [7] was the third of the Juno II launch vehicle, after it failed to carry Pioneer 3 into heliocentric orbit in December 1958, [8] [9] but succeeded in the same objective in March 1959, carrying the United States' first interplanetary mission, Pioneer 4 . [10] [11] S-1 was the first geocentric orbit launch attempt for the launch vehicle; its second attempt on 14 August 1959, carrying the Beacon 2 inflatable sphere experiment to low Earth orbit, also failed. [6] [12] Eventually, both the Juno II and a re-launch of the S-1 mission, designated Explorer 7 or S-1A, found success on 13 October 1959. [13] [14] The satellite, which ended its mission in August 1961, is still orbiting the Earth today. [12] [15]

See also

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References

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