2. NOAA’s GOES-R Spacecraft Jamison Hawkins Lockheed Martin Corporation

4. Music: Also Sprach Zarathustra by Richard Strauss performed by John Williams and the Boston Symphony Orchestra Philips, 1983

5. GOES-R Over 100 Remote Sensing Satellites More than 500 Instruments Successfully Built and Delivered: 50 Years of Delivering Earth Observation Advances

6. 5 2010 1980 Satcom 3R Aurora 1 Satcom 4 Spacenet-1 Spacenet-2 Satcom 1R Satcom 2R BS-2A GSTAR-1 ASC-1 Satcom Ku-2 GSTAR-2 BS-2B Satcom Ku-1 Satcom C1 ASTRA-1A GSTAR-3 PanAmSat-1 Spacenet-3R BS-3A GSTAR-4 ASTRA-1B Anik-E2 Spacenet-4 Aurora-2 BS-3B Anik-E1 NSS-K Satcom C4 Satcom C3 Telstar 401402R ACTS BS-3N Chinastar-1 AsiaSat 2 Koreasat EchoStar Inmarsat-3/F AMC Intelsat-VIII 12 NSS-803 45 NSS-806 12 101102 IIIIV 12345 123 AP Telkom I 1985199019952000 ABS-1 6 8 7 Nimiq-1 JCSAT-110 Iridium (89 buses) 4 3 ACeS Garuda-1 10 2005 IKONOS N-STAR c VII NSS-6 RCA Astro Electronics GE Astro Space Martin Marietta Astro Space Lockheed Martin CSS NSS-7 A2100 bus Legend EchoStar Koreasat 1958 SCORE 1st Communications Payload Nimiq-2 Rainbow-1 18 11 15 16 Between 1975 and 1980 BSE, Satcom 1, Satcom2, Anik-B ASTRA IKR ASTRA IL JCSAT 9, 10 JCSAT 11, 12 EchoStar X SIRIUS 4 BSAT-3a VINASAT 1 Satisfying Global Market Needs for Over 25 Years Our A2100-Based GOES-R Solution Provides Highest Value and Performance, A2100 spacecraft have accumulated 200 years of on-orbit operation without a failure 14

7. GOES-R Overview A collaborative development and acquisition –Flight Project - led by NASA –Ground Segment Project - led by NOAA Scheduled for launch in 2015 Six advanced instruments New and improved capabilities for –decreased lead times for severe weather warnings –better storm tracking capabilities –solar, space weather, and climate analyses –advanced products for aviation, transportation, commerce Extending the continuity of NOAA’s 40-year geostationary mission, GOES-R will be the next weather sentinel for monitoring threatening weather, and providing data for forecasting and environmental analyses

8. Satellite Driving Requirements Provide precision, stable space platforms at two operational geostationary orbital locations (75W and 135W) carrying the baseline instrument set Operational Mission - First Launch 2015: Provide continuity and improvements over the current system with spacecraft bus reliability of 0.81 after 10 years of on-orbit operation preceded by 5 years ground storage & up to 5 years on- orbit storage Spacecraft On-Orbit Life of 15 years with orbit East-West and North-South position maintained to within +/-0.1 degree. Support 9 station location changes Collect and transmit up to 140Mbps (coded) Instrument Payload data from each location continuously. Continue Rebroadcast function at L-Band up to 31 Mbps utilizing dual polarization Provide continuing and new services (Search & Rescue, Data Collection, EMWIN)

9. Visible & IR ImageryLighting MappingSpace Weather MonitoringSolar Imaging Advanced Baseline Imager (ABI) Geostationary Lightning Mapper (GLM) Space Environment In-Situ Sensor Suite (SEISS) Magnetometer Solar Ultra-Violet Imager (SUVI) Extreme UV/X-Ray Irradiance Sensors (EXIS) GOES-R is the next generation of NOAA geostationary satellites that will provide a major improvement in quality, quantity and timeliness of data collected. GOES-R Mission

10. ABI GLM SUVI Magnetometer Star trackers SEISS EXIS

11. ABI GLM SUVI Magnetometer Star trackers SEISS EXIS Greg Mandt – 1.8 m

12. GOES-R Spacecraft Configuration (External)

13. Notable Performance Elements Operates through daily station- keeping and momentum adjust maneuvers –Low risk station-keeping operations –Increased instrument availability –Decreased propellant required due to high efficiency thruster Yaw flip improves ABI radiometric response –Outage twice per year –Total time of noncompliance for instrument interface requirements <120 min per year Vibration Isolation for optical bench

14. Animation shows the vibration-isolation impact ABI and GLM are mounted on stiff optical bench –Dynamics are tunable to optimize system performance –Couple instrument motion to IMU and star trackers with low thermal distortion High-accuracy attitude determination system on the instrument optical bench –High accuracy star trackers –High-bandwidth, low-latency and low-noise IMU for effective motion compensation ABI & GLM Decoupled from Bus Design Elements Support Precision INR for Users Augmented attitude control array damping demonstrated with risk-reduction tests

15. Optical Bench Vibration Isolation Impact

16. GOES-R Satellite Production and Support Locations

17. NOAA’s GOES-R Spacecraft