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[[caption]]
Figure 5: Perseus B configuration, represented here by the Perseus proof-of-concept aircraft. Perseus B would carry fuel in its wing and have a turbocharged engine, and would be strengthend [[strengthened]] to a gross weight of 1,000 kg, allowing payloads up to 200 kg. An alternative configuration under study would have twin engines, for security on long missions, and sufficient propellor clearance for self-launching.
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