Areosynchronous Weather Imager

被引:0
作者
Puschell, Jeffery J. [1 ]
Lock, Robert [2 ]
机构
[1] Raytheon Space & Airborne Syst, 2000 East El Segundo Blvd,EO-E01-C150, El Segundo, CA 90245 USA
[2] Jet Prop Lab, Pasadena, CA USA
来源
REMOTE SENSING SYSTEM ENGINEERING VI | 2016年 / 9977卷
关键词
remote sensing; environmental satellite system; Mars; areosynchronous Mars orbit;
D O I
10.1117/12.2242301
中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
Mars is characterized by rapidly changing, poorly understood weather that is a concern for future human missions. Future Areosynchronous Mars Orbit (AMO) communication satellites offer possible platforms for Mars weather imagers similar to the geosynchronous Earth orbit (GEO) weather imagers that have been observing Earth since 1966. This paper describes an AReosynchronous Environmental Suite (ARES) that includes two imagers: one with two emissive infrared bands (10.8 mu m and 12.0 mu m) at 4 km resolution and the other with three VNIR bands (500 nm, 700 nm, 900 nm) at 1 km resolution. ARES stares at Mars and provides full disk coverage as fast as every 40 sec in the VNIR bands and every 2 min in the emissive bands with good sensitivity (SNR similar to 200 in the VNIR for typical radiances and NEDT similar to 0.2K at 180 K scene temperature in the emissive infrared). ARES size, mass, power and data rate characteristics are compatible with expectations for hosted payloads onboard future AMO communication satellites. Nevertheless, more work is needed to optimize ARES for future missions, especially in terms of trades between data rate, full disk coverage rate, sensitivity, number of spectral bands and spatial resolution and in study of approaches for maintaining accurate line of sight knowledge during data collection.
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页数:13
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