2 nd International space conference in Lithuania Space

- The leading enterprise and the world’s pre-eminent designer and operator of the middle-class

1. Provision of launch services of satellites designed by foreign companies. 2. Building of

Launch options: 1. As piggyback payload on satellites designed by the Samara Space Center.

Orbital parameters: Apogee – 575 км Perigee – 290 км Inclination– 64, 9˚ The

Orbital parameters: Near-circular Нnc = 300 km inclination i between 51, 8º and 98º

Multi-purpose platform to accommodate of Сub. SAT satellites, which supports : Ø Housing of

Key specifications: 1. Dimensions 620 х520 х485 mm; 2. Mass of the small satellite

Thank you for your attention Samara Space Centre 18, Zemets str. , Samara, 443009,

Slides: 9

Download presentation

2 nd International space conference in Lithuania «Space Economy in the Multipolar World» (SEMWO-2011) Samara Space Centre Feasibility of launching Cube. Sat small satellites in the Earth orbit Head of foreign economic division, Candidate of Economics A. V. SIDORENKO Doctor of Engineering, professor I. V. BELOKONOV www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86

- 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. www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 1

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. 3. Building of the Earth remote sensing satellites and accommodation of the foreign payload on them for its long-term operation in orbit. 4. Exchange of data acquired by the Earth remote sensing satellites. www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 2

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

Orbital parameters: Apogee – 575 км Perigee – 290 км Inclination– 64, 9˚ The launch is set for August 2012 Layout of Cube. Sat containers www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 4

Orbital parameters: Near-circular Нnc = 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 20 kg 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 minus 40 to +50°С ; - in-flight: from 40 to +100°С. www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 5

Multi-purpose platform to accommodate of Сub. SAT satellites, which supports : Ø Housing of containers (unified launch adapters), Ø Small satellite separation, Ø Monitoring of separation. Orbital parameters: Altitude from 500 km to 1500 km Inclination from 51, 8°to 98°. www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 6

Key specifications: 1. Dimensions 620 х520 х485 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 Нnc = 575 km; – inclination j = 64, 9˚; The small satellite is in non-controlled flight www. samspace. ru, e-mail: ved 878@samspace. ru, факс: +7 (846) 992 -64 -86 7

Thank you for your attention Samara Space Centre 18, Zemets str. , Samara, 443009, Russia Tel. : +7 (846) 955 -13 -61 Fax: +7 (846) 992 -64 -86 E-mail: ved 878@samspace. ru www. samspace. ru