Spaceborne Architecture
Spacecraft: AOS-P1 | AOS-I1 | AOS-I2
Spacecraft acronyms:
- AOS-P1 - Space Segment Polar
- 98° inclination (i.e., polar) orbit
- Sun synchronous
- 1:30 AM/PM equatorial crossing
- AOS-I (1 and 2) – Space Segment GPM
- 65° inclined orbit, similar to GPM (final inclination may be different)
International contributions are marked with flags. Other elements will be provided by NASA/US. Information regarding other candidate architectures considered for this mission.
| Instrument | Size | Description |
|---|---|---|
| AOS-P1 | ||
| Ka + W Doppler Radar | Medium satellite radar | W band Doppler, Ka band Doppler, 15km swath |
| Microwave Radiometer | Small satellite radiometer | 118, 183, 240, 310, 380, 660, 880 GHz |
| HSRL Lidar | Medium satellite lidar | 532nm HSRL, 1064nm backscatter |
| Multi-angle Polarimeter | Small-medium satellite polarimeter | 550km swath, 0.5km resolution |
| TIR Spectrometer | Small satellite spectrometer | Long wave infrared |
| UV-VIS Spectrometer | Small satellite spectrometer | Short wave infrared |
| AOS-I1 | ||
| W, Ku Doppler Radar | Small satellite radar | W band Doppler, Ku band Doppler |
| Camera | Small satellite camera | Stereo camera visible imaging |
| AOS-I2 | ||
| Backscatter Lidar | Small satellite lidar | 532nm, 1064nm backscatter |
| Microwave Radiometer | Small satellite radiometer | 118, 183, 240, 310, 380, 660, 880 GHz |
| Multi-angle Polarimeter | Small satellite polarimeter | 1130km swath, 1km resolution |
| Camera | Small satellite camera | Stereo camera visible imaging |
Launch: AOS-I1 and AOS-I2 will launch mid-2028, followed by AOS-P1 in early 2030. Acronyms: HSRL: High Spectral Resolution Lidar; TIR: Terminal Imaging Radar; UV/VIS: Ultraviolet/Visible.