Www.samspace.ru, e-mail: [email protected], факс: +7 (846) 992-64-86.

www.samspace.ru, e-mail: [email protected], 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: [email protected], 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.

www.samspace.ru, e-mail: [email protected], факс: +7 (846) 992-64-86 2

4. 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.

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Launch options:

1.As piggyback payload on satellites designed by the Samara Space

Center.

2.By Soyuz carrier orbital stage.

Orbital parameters:

Apogee – 575 кмPerigee – 290 кмInclination– 64,9˚

The launch is set for August 2012

www.samspace.ru, e-mail: [email protected], факс: +7 (846) 992-64-86

Layout of CubeSat containers

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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 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.


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°.


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 Нnc = 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, 443009, RussiaTel.: +7 (846) 955-13-61Fax: +7 (846) 992-64-86 +7 (846) 992-64-86

E-mail: [email protected]

Www.samspace.ru, e-mail: [email protected], факс: +7 (846) 992-64-86.

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