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Presentation transcript:

факс: +7 (846)

- The leading enterprise and the world’s pre-eminent designer and operator of the middle-class launch vehicles, the Earth remote sensing space systems and unmanned satellites for application research. - Possesses rich experience of participation in large-scale international projects on development of outer space for peaceful purposes. факс: +7 (846)

1. Provision of launch services of satellites designed by foreign companies. 2. Building of satellites accommodating joint fundamental or applied experiments to be conducted under microgracity conditions in the sphere of material study, biology and medicine. факс: +7 (846) Exchange of data acquired by the Earth remote sensing satellites. 3. Building of the Earth remote sensing satellites and accommodation of the foreign payload on them for its long-term operation in orbit.

3 Launch options: 1.As piggyback payload on satellites designed by the Samara Space Center. 2.By Soyuz carrier orbital stage.

Orbital parameters: Apogee – 575 км Perigee – 290 км Inclination– 64,9˚ The launch is set for August факс: +7 (846) Layout of CubeSat containers 4

5 факс: +7 (846) Orbital parameters: Near-circular Н nc = 300 km inclination i between 51,8º and 98º Small satellite basic requirements: 1. Permissible total mass of small satellite H/W (including container) is 20kg maximum. 2. Small satellite separation speed is between 0,1 and 0,6 m/s. 3. Thermal environment around small satellite fixed on the intermediate bay: - at launch: from minus40 to +50°С ; - in-flight: from 40 to +100°С.

6 факс: +7 (846) Multi-purpose platform to accommodate of СubSAT satellites, which supports :  Housing of containers (unified launch adapters),  Small satellite separation,  Monitoring of separation. Orbital parameters: Altitude from 500km to 1500km Inclination from from51,8°to 98°.

7 факс: +7 (846) Key specifications: 1.Dimensions 620х520х485 mm; 2.Mass of the small satellite with adapter – 60 kg. 3.Orbital life – 3 years maximum; 4.Initial parameters of the operating orbit : – near-circular Н nc = 575 km; – inclination j = 64,9˚; The small satellite is in non-controlled flight

Thank you for your attention Samara Space Centre 18, Zemets str., Samara, , Russia Tel.: +7 (846) Fax: +7 (846) (846)