Integral launch

The first stage of the booster has six engines. They ignited 1.6 seconds before lift-off. After two minutes flight, the ignition of the four engines of stage two occurred. About four minutes later the third-stage main engine ignites.

These three booster stages use nitrogen tetroxide and unsymmetrical dimethylhydrazine as propellants. They placed the upper section with the spacecraft into a low parking orbit with an inclination of 51.6° with respect to the equatorial plane.

About 50 minutes later, the upper stage was ignited. This was powered by a restartable, liquid oxygen-synthetic kerosene propulsion system. The upper stage put the satellite into a highly eccentric transfer orbit with a perigee altitude of about 700 kilometres. At the end of the upper-stage burn, the satellite separated.

Then Integral's own propulsion system brought the spacecraft to its operational 72-hour orbit with an initial perigee height of 10 000 kilometres and the apogee height of 153 000 kilometres. The perigee height increases throughout the mission to about 13 000 kilometres after five years. In addition to the orbit shape, the inclination also changes drastically to 85° after five years.

The high and eccentric orbit guarantees long periods of uninterrupted observation with nearly constant background and away from trapped radiation in Earth's proton and electron belts. In this way, scientists can use 90% of the time spent in the orbit provided by the Russian rocket for scientific observations above an altitude of 40 000 kilometres. The orbital period with its 72 hours is a multiple of 24 hours which guarantees an optimal coverage pattern from the ground stations. This coverage is continuous for Integral's orbit for all revolutions and allows repetitive working shifts on ground.

In its four-stage configuration, Proton is regularly used to launch spacecraft into geosynchronous trajectories. As a three-stage vehicle it primarily launches large 'space station' type payloads into low-Earth orbit. In November 1998, a Proton rocket put the first component for the International Space Station (ISS) into orbit. In the future, the Proton will be a crucial asset in deploying ISS.

Production of the first two-stage Proton model started in 1962. The four-stage rocket was originally developed to fly by the Moon with a manned capsule. Today, International Launch Services, a joint venture between the Russian companies Khrunichev and RSC Energia and American Lockheed Martin commercially market launch services of western satellites on the Proton. In April 1996 an Astra broadcast satellite was the first Western spacecraft to be carried by a Russian Proton rocket. Many others have followed, for example, the Iridium satellites for mobile telephony.