Environmental & Social Report - Subaru

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Reference Fiscal 2010 Fuel Economy Standards (10-15 Mode) Gasoline Passenger Cars Equivalent inertia weight (kg) —750 Lower limit Vehicle weight (kg) Upper limit 702 Fiscal 2010 fuel economy standards (km/l) 21.2 — 875 703 827 18.8 1000 828 1015 17.9 1250 1016 1265 16.0 1500 1266 1515 13.0 1750 1516 1765 10.5 2000 1766 2015 8.9 2250 2016 2265 7.8 2500— 2266 — 6.4 Gasoline Mini-Sized Trucks Equivalent inertia weight (kg) —750 Lower limit Vehicle weight (kg) Upper limit 702 Vehicle structure (Note) Structure A Structure B AT 18.9 16.2 Fiscal 2010 fuel economy standards (km/l) MT 20.2 17.0 — Structure A 16.5 18.0 875 703 827 Structure B 15.5 16.7 1000— 828 — — 14.9 15.5 Maximum load capacity Note: Structure A 0.3 Gross vehicle weight FWD (front-wheel drive) vehicles or FWD-based 4WD vehicles (excluding trucks); Pleo vans Structure BVehicles other than Structure A; Sambar vans and trucks Reference Exhaust Emission Regulation Values, Low Emission Vehicle Authorization Standard by the Ministry of Land, Infrastructure and Transport New Short-Term Regulations for Gasoline and LPG Passenger Cars 2000 exhaust emission regulations 2000 standard emission 25% reduction level 2000 standard emission 50% reduction level 2000 standard emission 75% reduction level 2005 exhaust emission regulations 2005 standard emission 50% reduction level 2005 standard emission 75% reduction level CO 0.67 0.67 0.67 0.67 CO 1.15 1.15 1.15 10-15 mode (g/km) HC 0.08 0.06 0.04 0.02 NMHC 0.05 0.025 0.013 NOx 0.08 0.06 0.04 0.02 CO 19.0 19.0 19.0 19.0 New Long-Term Regulations for Gasoline and LPG Passenger Cars Combined mode (g/km) NOx 0.05 0.025 0.013 11 mode (g/test) HC 2.20 1.65 1.10 0.55 Combination 10-15 mode & 11 mode 10-15 mode & 11 mode 10-15 mode & 11 mode NOx 1.40 1.05 0.70 0.35 Remarks Good low emission vehicle Excellent low emission vehicle Ultra low emission vehicle Remarks U-LEV SU-LEV New Short-Term Regulations for Gasoline and LPG Mini-Sized Trucks 2002 exhaust emission regulations 2000 standard emission 25% reduction level 2000 standard emission 50% reduction level 2000 standard emission 75% reduction level 2007 exhaust emission regulations 2005 standard emission 50% reduction level 2005 standard emission 75% reduction level CO 3.30 3.30 3.30 3.30 CO 4.02 4.02 4.02 10-15 mode (g/km) HC 0.13 0.10 0.07 0.03 NMHC 0.05 0.025 0.013 NOx 0.13 0.10 0.07 0.03 CO 38.0 38.0 38.0 38.0 New Long-Term Regulations for Gasoline and LPG Mini-Sized Trucks Combined mode (g/km) NOx 0.05 0.025 0.013 11 mode (g/test) HC 3.50 2.63 1.75 0.88 Combination 10-15 mode & 11 mode 10-15 mode & 11 mode 10-15 mode & 11 mode NOx 2.20 1.65 1.10 0.55 Remarks Good low emission vehicle Excellent low emission vehicle Ultra low emission vehicle Remarks U-LEV SU-LEV
1 <strong>Environmental</strong> <strong>Report</strong> Development Phase/Products —Aerospace, Industrial Products and Eco Technologies Companies— Development Phase/Products —Aerospace, Industrial Products and Eco Technologies Companies— Aerospace Company The Aerospace Company has been contributing with a remarkable participation in the national government Millennium Project ✽1 in Japan, mostly on the meteorological issue of the greenhouse effect, which may cause global warming. We are now developing two unmanned prototype airships to utilize stratospheric platform technology. In the future, the goal of the stratospheric airship is to realize broad applications of telecommunications, broadcasting, and remote sensing observations. The Stratospheric Platform Airship is expected to have a very long geostationary fl ight duration at an altitude of 20 km by benefi ting from the stable, calm winds and sunshine. Currently, we are going ahead with the design and manufacturing stage for two prototypes of the airship (48-meter, non-powered, balloon-like, high-altitude, fl ighttesting model and a 68-meter unmanned reusable low-attitude model) under a contract with the National Aerospace Laboratory of Japan. In future production models, which will follow these prototype airships, we will install high effi ciency solar and fuel cells for pollution-free power sources, which are mandatory for a long stay in the stratosphere. It is anticipated that a new type of service business using undeveloped traffi c- free airspace in the stratosphere will grow quickly and broadly in areas useful to the public and commercial market. In the information and communications area, advanced information services for next-generation cellular phones, digital high defi nition television broadcasting, and telematics are strongly expected to develop as new businesses. In the area of global observation, the Stratospheric Platform Airship will enable long, continuous observation in support of rescue/restoration/reconstruction projects by its wide coverage area for serious disasters, as well as monitoring and surveys of land, sea, and atmospheric pollution. After one of the stratospheric airship production models enters service, it will cover an area with a radius of more than 100 km using next generation remote sensing and observation for high resolution and accuracy. Actualization of high-speed communication in a wider service area than ground cellular systems Realization of smooth communication with almost no transmission time delay, and downsized antenna and power saving of communications terminals Utilization of wide-area communication and broadcasting services using the platform network by multiple airships Digital broadcasting Communication and broadcasting Ultra high-speed Internet Atmosphere (ozone layer) sampling, etc. Observation of the globe Ocean and land Disaster monitoring Hurricanes and tornados Contribution to prediction of global changes by observing the land, sea, and the stratosphere Industrial applications in agriculture, forestry, fishery, traffic and transport, and disaster support by continuous local observation Forest fires on mountains Cellular phone Mobile communication (G3 & G4) (navigation and telematics) ✽1. Millennium Project: Funded by the national government. Joint industry-academia-government projects are planned in the three areas of informatization, aging society, and environmental measures, which are very important and urgent to the Japanese economy and society so as to cope with current issues and to keep current with technological innovation that creates new industries. Flight Test of 48-Meter Model Launching In August 2003, a fl ight test of the 48-meter, non-powered, balloon-like, high-altitude fl ight-testing model was conducted at Hitachi Seaport in Ibaragi Prefecture. Although the test fl ight had been postponed due to bad weather, it was clear with a mild wind on that day. Under the best conditions, the test model fl ew stably in accordance with the anticipated simulation: launch (at 3:21 a.m.), climb, stay (reached altitude: about 16.4 km), descend, and land on the water (at 5:15 a.m.). We accomplished a signifi cant goal by checking the performance of the model and the validity of the simulation. The horizon was photographed from the stratosphere by a camera mounted on the airship model. (Seaside) Bottom of the test model (airship) (Sky side)
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