![]() SOLRAD 4 satellite | |
Names | GRAB 3 SOLar RADiation 4 SR 4 GREB 3 |
---|---|
Mission type | Solar X-Rays |
Operator | United States Naval Research Laboratory (USNRL) |
COSPAR ID | 1962-F02 (SR4GREB) |
Mission duration | Failed to orbit |
Spacecraft properties | |
Spacecraft type | SOLRAD |
Manufacturer | Naval Research Laboratory (NRL) |
Launch mass | 25 kg (55 lb) |
Dimensions | 51 cm (20 in) |
Start of mission | |
Launch date | 24 January 1962, 09:30GMT |
Rocket | Thor-Ablestar |
Launch site | Cape Canaveral,LC-17B |
Contractor | Douglas Aircraft Company |
End of mission | |
Decay date | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit (planned) |
Regime | Low Earth orbit |
Perigee altitude | 930 km |
Apogee altitude | 930 km |
Inclination | 66.80° |
Period | 103.00 minutes |
SOLRAD (SOLar RADiation) 4 was asolar X-rays,ultraviolet, and electronic surveillance satellite. Developed by theUnited States Navy'sUnited States Naval Research Laboratory (USNRL), it was the fourth in both theSOLRAD and theGRAB (Galactic Radiation and Background) programs.
The satellite was to be orbited along withionospheric study satelliteLOFTI-2, theUnited States Army's range calibration satelliteSECOR, Navy surveillance calibration satelliteSurcal, and theUniversity of Iowa'sVan Allen radiation belts-studyingInjun 2 satellite. This unprecedented five-in-one mission, called "Composite 1" and "Buckshot", ended in failure on 24 January 1962 after itsThor-Ablestar's second stage failed to deliver the payloads to orbit.
TheUnited States Navy'sUnited States Naval Research Laboratory (USNRL) established itself as a player early in theSpace Race with the development and management ofProject Vanguard (1956–1959),[1] America's first satellite program. After Vanguard, the Navy's next major goal was to use the observational high ground ofEarth's orbit to survey Sovietradar locations andfrequencies. This first space surveillance project was called "GRAB", later expanded into the more innocuousbackronym, Galactic Radiation And Background.[2] As American space launches were not classified until late 1961,[3][4] a cover mission sharing thesatellite bus was desired to conceal GRAB's electronic surveillance mission from its intended targets.[2]
The field of solar astronomy provided such cover. Since the invention of the rocket, astronomers had wanted to fly instruments above the atmosphere to get a better look at theSun. The Earth's atmosphere blocks large sections of sunlight'selectromagnetic spectrum, making it impossible to study the Sun's X-ray and ultraviolet output from the ground. Without this critical information, it was difficult to model the Sun's internal processes, which in turn inhibited stellar astronomy in general.[5]: 5–6 On a more practical level, it was believed that solar flares directly affected the Earth'sthermosphere, disruptingradio communications. The U.S. Navy wanted to know when its communications were going to become unreliable or compromised.[2]Sounding rockets had shown that solar output was unpredictable and fluctuated rapidly. A long-term, real-time observation platform above the Earth's atmosphere – in other words, asatellite – was required to properly chart the Sun's radiation, determine its effects on theEarth, and correlate it with ground-based observations of the Sun in other wavelengths of light.[5]: 63
Thus, the SOLRAD project was conceived to address several NRL goals at once:
SOLRAD 4 had two successful predecessors inSOLRAD 1 andSOLRAD 3, both of which made significant contributions to the understanding of ultraviolet and X-ray astronomy in the previous two years,[5]: 64–68 and which returned an abundance of intelligence on Soviet air defense radar installations.[9]
Like its predecessors, SOLRAD 4 was roughly spherical, modeled on theVanguard satellite (which also had been developed by theUnited States Naval Research Laboratory), and included both the scientific SOLRAD and the electronic surveillance GRAB packages within the same satellite. Mass of 25 kg,[10] the fourth in the SOLRAD series was more heavily instrumented than prior SOLRADS. Instead of one X-ray photometer, likeSOLRAD 1 andSOLRAD 2, or two, likeSOLRAD 3, it carried four X-ray photometers, allowing it to detect more intense and higher energy X-rays. Three of the photometers were shielded againstVan Allen radiation belts (which could spoil results) by magnets, as had been done on earlier missions. The fourth was protected by aberyllium shield. It was hoped that SOLRAD 4 would not only conduct basic research into solar X-ray astronomy, but also determine the hazard hard X-rays posed toastronauts andsatellites.[11]
Another point of difference between SOLRAD 4 and its predecessors was its fourLyman-alpha detectors.[11] Used for measuring ultraviolet radiation, two such detectors had been included on SOLRAD 1 and SOLRAD 2 to determine the impact of solar ultraviolet on radio reception.[12] None had been measured, and the detectors had been deleted from SOLRAD 3. They were reinstated on SOLRAD 4 not for solar study, but for night-time measurement to see if ambient Lyman-alpha radiation constituted a threat to astronauts and satellites.[11]
On 24 January 1962 at 09:30 GMT,[13] SOLRAD 4 was launched viaThor-Ablestar[10] fromCape Canaveral LC-17B[13] along withionospheric study satelliteLOFTI 2, theUnited States Army's range calibration satelliteSECOR, Navy surveillance calibration satelliteSURCAL, and the University of Iowa'sVan Allen radiation belts-studyingInjun 2 satellite. This unprecedented five-in-one mission, called "Composite 1" and "Buckshot", ended in failure: the Thor first stage performed properly, but the Ablestar second stage developed insufficient velocity to attain orbit. While the exact cause was not immediately known, there were indications that the Ablestar had not separated cleanly from the Thor stage, instead tumbling end over end.[14] The estimated cost of the lost rocket and payload was US$3.5 million.[15]
The SOLRAD/GRAB series flew once more (unsuccessfully), finishing with theSOLRAD 4B mission launched 26 April 1962.[2] In 1962, all U.S. overhead reconnaissance projects were consolidated under theNational Reconnaissance Office (NRO), which elected to continue and expand the GRAB mission starting July 1962[16] with a next-generation set of satellites, code-namedPOPPY.[10] With the initiation of POPPY, SOLRAD experiments would no longer be carried on electronic spy satellites; rather, they would now get their own satellites, launched alongside POPPY missions to provide some measure of mission cover.[13] Starting withSOLRAD 8, launched in November 1965, the final five SOLRAD satellites were scientific satellites launched singly, three of which were also given NASAExplorer program numbers. The last in this final series of SOLRAD satellites flew in 1976. In all, there were thirteen operational satellites in the SOLRAD series.[2] The GRAB program was declassified in 1998.[9]
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