SOLRAD 4

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, 09:30 GMT
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 ← SOLRAD 3 SOLRAD 4B → GRAB ← GRAB 2 (5th GRAB mission) →

SOLRAD (SOLar RADiation) 4 was a solar X-rays, ultraviolet, and electronic surveillance satellite. Developed by the United States Navy's United States Naval Research Laboratory (USNRL), it was the fourth in both the SOLRAD and the GRAB (Galactic Radiation and Background) programs.

The satellite was to be orbited along with ionospheric study satellite LOFTI-2, the United States Army's range calibration satellite SECOR, Navy surveillance calibration satellite Surcal, and the University of Iowa's Van Allen radiation belts-studying Injun 2 satellite. This unprecedented five-in-one mission, called "Composite 1" and "Buckshot", ended in failure on 24 January 1962 after its Thor-Ablestar's second stage failed to deliver the payloads to orbit.

The United States Navy's United States Naval Research Laboratory (USNRL) established itself as a player early in the Space Race with the development and management of Project Vanguard (1956–1959),^[1] America's first satellite program. After Vanguard, the Navy's next major goal was to use the observational high ground of Earth's orbit to survey Soviet radar locations and frequencies. This first space surveillance project was called "GRAB", later expanded into the more innocuous backronym, Galactic Radiation And Background.^[2] As American space launches were not classified until late 1961,^[3][4] a cover mission sharing the satellite 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 the Sun. The Earth's atmosphere blocks large sections of sunlight's electromagnetic 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's thermosphere, disrupting radio 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, a satellite – was required to properly chart the Sun's radiation, determine its effects on the Earth, 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:

• to make the first long-term continuous observations of the sun in ultraviolet and X-ray light, and to correlate these measurements with ground-based observations.^{[5]: 64–65}
• to evaluate the level of hazard posed by ultraviolet and X-ray radiation.^[6]
• to better understand the effect of solar activity (including solar flares) on radio communications.^[7][8]
• to cheaply and efficiently produce a satellite for the GRAB surveillance mission by using a proven design.^[2]
• to obscure the GRAB mission under a scientific cover.^[2]

SOLRAD 4 had two successful predecessors in SOLRAD 1 and SOLRAD 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 the Vanguard satellite (which also had been developed by the United 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, like SOLRAD 1 and SOLRAD 2, or two, like SOLRAD 3, it carried four X-ray photometers, allowing it to detect more intense and higher energy X-rays. Three of the photometers were shielded against Van Allen radiation belts (which could spoil results) by magnets, as had been done on earlier missions. The fourth was protected by a beryllium 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 to astronauts and satellites.^[11]

Another point of difference between SOLRAD 4 and its predecessors was its four Lyman-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 via Thor-Ablestar^[10] from Cape Canaveral LC-17B^[13] along with ionospheric study satellite LOFTI 2, the United States Army's range calibration satellite SECOR, Navy surveillance calibration satellite SURCAL, and the University of Iowa's Van Allen radiation belts-studying Injun 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 the SOLRAD 4B mission launched 26 April 1962.^[2] In 1962, all U.S. overhead reconnaissance projects were consolidated under the National Reconnaissance Office (NRO), which elected to continue and expand the GRAB mission starting July 1962 ^[16] with a next-generation set of satellites, code-named POPPY.^[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 with SOLRAD 8, launched in November 1965, the final five SOLRAD satellites were scientific satellites launched singly, three of which were also given NASA Explorer 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]

• General information on the SOLRAD project
• General information on the GRAB project