Data relating to Flight 170 by H. Lantéri - Astrium - EADS

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3. Payload (end) The satellite * Dimensions * Mass * Power • 3.75 x 1.8 x 2.3 m (hxLxl) • 36.9 m with solar arrays deployed • lift-off • dry 4,100 kg (forecast) 1,740 kg • 9,800 W (en début de vie) - 2 solar arrays • NiH2 batteries (96 AH) * Propulsion • bi-liquid propellant with an apogee engine (400N). * Stabilization • Slow spin (1,5°/s) on separation • Triple axis stabilization in orbit * Transmission capability • Ku-band payload (38 transponders) * Orbital position • 13° E * Ground coverage • Europe Scheduled service life: 15 years Test in acoustic chamber Photo Alcatel Alenia Space 16
4. Launch campaign The Ariane 5 main cryogenic stage (EPC) in the integration dock at Les Mureaux, France, in course of preparation for containerization. Copyright: EADS ST photo: Studio Bernot Ariane 5 ESC flight thrust frame at EADS-LV Les Mureaux, before departure for Astrium in Bremen. Copyright: EADS ST photo: Studio Bernot The main cryogenic stage loading on board the "Toucan" in the port of Le Havre for shipment to French Guiana. Copyright: EADS ST photo: JL 17
Page 1 and 2: Kourou February 200 Data relating t
Page 3 and 4: 1. Introduction Flight 170 is the 2
Page 5 and 6: 2. Launcher L527 (continued) Compar
Page 7 and 8: 2. Launcher L527 (continued) ESC-A
Page 9 and 10: 2. Launcher L527 (continued) Flight
Page 11 and 12: 2. Launcher L527 (continued) Phase
Page 13 and 14: 3. Payload SPAINSAT Program and mis
Page 15: 3. Payload (continued) HOT BIRD 7A
Page 19 and 20: 4. Launch campaign (end) Kourou: tr
Page 21 and 22: 6. Final countdown The final countd
Page 23 and 24: 6. Final countdown - Synchronized s
Page 25 and 26: 7. Flight sequence time /H 0 (s) ti
Page 27 and 28: 8. EADS SPACE Transportation and th

Data relating to Flight 170 by H. Lantéri - Astrium - EADS

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