The USA V-2 period scientists J. D. Purcell, C. Y. Johnson, and Dr. F. S. Johnson among those recovering instruments from a V-2 used for upper atmospheric research above the New Mexico desert. This is V-2 number 54, launched January 18, 1951 (photo by Dr. Richard Tousey, NRL). The beginning of the search for X-ray sources from above the Earth's atmosphere was on
August 5, 1948 12:07 GMT. A US Army
V-2 as part of
Project Hermes was launched from
White Sands Proving Grounds Launch Complex (LC) 33. In addition to carrying experiments of the US
Naval Research Laboratory for cosmic and solar radiation, temperature, pressure, ionosphere, and photography, there was on board a solar X-ray test detector, which functioned properly. The missile reached an apogee of 166 km. As part of a collaboration between the US Naval Research Laboratory (NRL) and the Signal Corps Engineering Laboratory (SCEL) of the University of Michigan, another V-2 (V-2 42 configuration) was launched from White Sands LC33 on December 9, 1948 at 16:08 GMT (09:08 local time). The missile reached an apogee of 108.7 km and carried aeronomy (winds, pressure, temperature), solar X-ray and radiation, and biology experiments. On January 28, 1949, an NRL X-ray detector (Blossom) was placed in the nose cone of a
V-2 rocket and launched at
White Sands Missile Range in New Mexico. X-rays from the Sun were detected. Apogee: 60 km. A second collaborative effort (NRL/SCEL) using a V-2 UM-3 configuration launched on April 11, 1949 at 22:05 GMT. Experiments included solar X-ray detection, apogee: 87.4 km. NRL Ionosphere 1 solar X-ray, ionosphere, meteorite mission launched a V-2 on September 29, 1949 from White Sands at 16:58 GMT and reached 151.1 km. Using V-2 53 configuration a solar X-ray experiment was launched on February 17, 1950 from White Sands LC 33 at 18:01 GMT reaching an apogee of 148 km. The last V-2 launch number TF2/TF3 came on August 22, 1952 07:33 GMT from White Sands reaching an apogee of 78.2 km and carried experiments • solar X-ray for NRL, • cosmic radiation for the National Institute of Health (NIH), and • sky brightness for the Air Research and Development Command.
Aerobee period The first successful launch of an
Aerobee occurred on May 5, 1952 13:44 GMT from
White Sands Proving Grounds launch complex LC35. It was an Aerobee RTV-N-10 configuration reaching an apogee of 127 km with NRL experiments for solar X-ray and ultraviolet detection. On April 19, 1960, an
Office of Naval Research Aerobee Hi made a series of X-ray photographs of the Sun from an altitude of 208 km. The mainstay of the US IGY rocket stable was the Aerobee Hi, which was modified and improved to create the Aerobee 150. An
Aerobee 150 rocket launched on June 12, 1962 detected the first X-rays from other celestial sources (Scorpius X-1).
USSR V-2 derivative launches Starting on June 21, 1959 from Kapustin Yar, with a modified
V-2 designated the R-5V, the USSR launched a series of four vehicles to detect solar X-rays: a R-2A on July 21, 1959 and two R-11A at 02:00 GMT and 14:00 GMT.
Skylark The British
Skylark was probably the most successful of the many sounding rocket programs. The first launched in 1957 from
Woomera, Australia and its 441st and final launch took place from
Esrange, Sweden on 2 May 2005. Launches were carried out from sites in Australia, Europe, and South America, with use by
NASA, the European Space Research Organisation (
ESRO), and
German and
Swedish space organizations. Skylark was used to obtain the first good-quality X-ray images of the solar corona. The first X-ray surveys of the sky in the Southern Hemisphere were provided by Skylark launches. from
Hammaguira, LC Blandine carrying experiments to measure UV and X-ray intensities and the FU110 to measure UV intensity from the
atomic H (Lyman-α) line, and again on November 4, 1964.
Early satellites satellite at the
National Cryptologic Museum. The satellites carried two sets of instruments: an unclassified experiment (called
Solrad) and a then-classified payload to collect electronic intelligence (
ELINT) (called Tattletale). The SOLar RADiation satellite program (SOLRAD) was conceived in the late 1950s to study the Sun's effects on Earth, particularly during periods of heightened solar activity.
Solrad 1 was launched on June 22, 1960 aboard a
Thor Able from
Cape Canaveral at 1:54 a.m. EDT. As the world's first orbiting astronomical observatory,
SOLRAD I determined that radio fade-outs were caused by solar X-ray emissions. Its orbital period was ~95 min. The spacecraft had a spin rate of 0.5 rps. On board was a hard X-ray detector (27-189 keV) with a 5.1 cm2 NaI(Tl) scintillator, collimated to 17° × 23° FWHM. The system had 4 energy channels (separated 27-49-75-118-189 keV). The detector spun with the spacecraft on a plane containing the Sun direction within ± 3.5°. Data were read with alternate 70 ms and 30 ms integrations for 5 intervals every 320 ms.
TD-1A was put in a nearly circular polar
Sun-synchronous orbit, with apogee 545 km, perigee 533 km, and inclination 97.6°. It was ESRO's first 3-axis stabilized satellite, with one axis pointing to the Sun to within ±5°. The optical axis was maintained perpendicular to the solar pointing axis and to the orbital plane. It scanned the entire celestial sphere every 6 months, with a great circle being scanned every satellite revolution. After about 2 months of operation, both of the satellite's tape recorders failed. A network of ground stations was put together so that real-time telemetry from the satellite was recorded for about 60% of the time. After 6 months in orbit, the satellite entered a period of regular eclipses as the satellite passed behind the Earth—cutting off sunlight to the solar panels. The satellite was put into hibernation for 4 months, until the eclipse period passed, after which systems were turned back on and another 6 months of observations were made.
TD-1A was primarily a UV mission however it carried both a cosmic X-ray and a gamma-ray detector. TD-1A reentered on January 9, 1980. ==Surveying and cataloging X-ray sources==