'KAIKS' Space-Complex is designed for performing the following tasks:
- Register high-speed impact parameters of meteoric and man-caused particles with the spherical surface of SC 'KAIKS' sensor, record the calculated results of the impacts for further transmission to the ground stations via radiotelemetric channels;
- Conduct dynamic tracking of density changes in upper atmosphere in the altitudes from 200 to 1000 km;
- Evaluate aerodynamic properties of objects in space.
Orbital injection of SC 'KAIKS' is carried out as secondary payload on 'Resurs'/'Foton' carrier with further separation.
Upon separation SC 'KAIKS' is put on autonomous non-oriented flight. The data transmission is done in three sessions per orbit in automatic mode.
Transmitted telemetrical data is received by the ground measuring stations.

Project execution stages:
1. Inject 'KAIKS-1' into orbit up to 400 km in order to verify operating capabilities of scientific equipment, design and fabrication method for capacitor-based sensors as well as zero-impact disagreement system and board system.
2. Inject 'KAIKS-2' with advanced equipment set into orbit up to 1000 km using its own booster.

1 - "KAIKS", 2 - Base satellite (Resurs/Foton)
3-Ballistic analog body
4-Booster (for 'KAIKS-2')
5-Sensor cover
6.1nstrumental container

Technical Requirements:

- particle mass range, g .................10e-9...1

- particle speed range, m/s ............10..3x10e-4