*** Welcome to piglix ***

INTEGRAL1

International Gamma-Ray Astrophysics Laboratory (INTEGRAL)
INTEGRAL 3D image
Artist's view of INTEGRAL spacecraft
Mission type Astronomy
Operator ESA  / RKA  / NASA
COSPAR ID 2002-048A
SATCAT no. 27540
Website sci.esa.int/integral/
Mission duration 14 years, 7 months and 23 days elapsed
Spacecraft properties
Manufacturer Alenia Spazio
Launch mass ~ 4,000 kg (8,800 lb)
Dry mass ~ 3,450 kg (7,610 lb)
Payload mass ~ 2,000 kg (4,400 lb)
Dimensions 5 m × 2.8 m × 3.2 m (16.4 ft × 9.2 ft × 10.5 ft)
Start of mission
Launch date 17 October 2002, 01:33 UTC (2002-10-17UTC01:33Z)
Rocket Proton-K Blok-DM2
Launch site Baikonur 200/39
Contractor Roscomos
Orbital parameters
Reference system Geocentric
Regime Highly elliptical
Semi-major axis 87,941 kilometres (54,644 mi)
Perigee 6,281.9 kilometres (3,903.4 mi)
Apogee 156,859.1 kilometres (97,467.7 mi)
Inclination 54.0 degrees
Period 4,325.6 minutes
Epoch 27 January 2015, 17:47:58 UTC
Main telescope
Type Coded mask telescope
Diameter 3.7 metres (12 ft)
Focal length ~ 4 metres (13 ft)
Collecting area 500 cm2 (78 sq in) (SPI, JEM-X)
3,100 cm2 (480 sq in) (IBIS)
Wavelengths 15 keV to 10 MeV (main)
3 to 35 keV (JEM-X)
500 to 580 nm (OMC)

INTEGRAL mission insignia
ESA astrophysics insignia for the INTEGRAL mission

Rosetta →

INTEGRAL mission insignia
ESA astrophysics insignia for the INTEGRAL mission

INTErnational Gamma-Ray Astrophysics Laboratory (INTEGRAL) is a currently operational space telescope for observing gamma rays. It was launched by the European Space Agency into Earth orbit in 2002, and is designed to detect some of the most energetic radiation that comes from space. It was the most sensitive gamma ray observatory launched before Fermi.

INTEGRAL is an ESA mission in cooperation with the Russian Space Agency and NASA. It has had some notable successes, for example in detecting a mysterious 'iron quasar'. It has also had success in investigating gamma-ray bursters and evidence for black holes.

Because gamma rays and X-rays cannot penetrate Earth's atmosphere, direct observations must be made from space. INTEGRAL was launched from Baikonur spaceport, in Kazakhstan. The 2002 launch aboard a Proton-DM2 rocket achieved a 700 km perigee. The onboard thrusters then raised the perigee out of the residual atmosphere, and the worst regions of the radiation belts. The apogee was trimmed with the thrusters to synchronize with Earth's rotation, and thus, the satellite's ground stations.

INTEGRAL's operational orbit has a period of 72 hours, and has a high eccentricity, with perigee close to the Earth at 10,000 km, within the magnetospheric radiation belt. However, most of each orbit is spent outside this region, where scientific observations may take place. It reaches a furthest distance from Earth (apogee) of 153,000 km. The apogee was placed in the northern hemisphere, to reduce time spent in eclipses, and maximize contact time over the ground stations in the northern hemisphere.


...
Wikipedia

...