Содержание
- 2. RUSSIAN HYDROMETEOROLOGICAL SATELLITE SYSTEM METEOR №1 METEOR №2 METEOR №3 Oceanographical ELECTRO №2 (14° E.) ELECTRO
- 3. Russian Earth Observation Satellites Program 2006-2015 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015
- 4. ELECTRO-L General Design • Three-axis high-precision stabilization • In-orbit mass - 1500 kg • Payload mass
- 5. MSU-GS Basic Performance Characteristics 10 Lifetime of basic and reserve units (years) 9. ≤ 88 Weight
- 6. METEOR-M General Design • In-orbit mass – 2700 kg • Payload mass – 1200 kg •
- 7. METEOR-M Mission Objectives and Basic Instruments Instrument * - to be launched on board METEOR-M №2
- 8. RESURS-DK General Design RESURS-DK Instruments Payload • In-orbit mass - 6570 kg • Payload mass -
- 9. 3 Main centers: Europe (Moscow-Obninsk-Dolgoprudny) Siberia (Novosibirsk) Far-East (Khabarovsk) ∙ - 68 Local centers Roshydromet Satellite
- 11. Скачать презентацию