The engine is mounted amidships and it features an unusual folding propeller which is stowed inside the aircraft's nose-cone when the engine is not in use. The Stemme S10 also has several unusual features such as a tailwheel undercarriage and a side-by-side cockpit. It does not have a tow hook connection so it must self-launch. The two main wheels retract and lower electrically, though they can also be lowered manually if needed. There is an option to fold wings to reduce hangar span to 11.4 m (37 ft 5 in). The engine restart time is 5 seconds. A solar panel can provide additional electrical power during long flights. It has a steerable tailwheel, Schempp-Hirth spoilers and optional winglets. The current variant, the S10-VT, has a variable-pitch propeller which allows more power during take off, and a new turbocharged Bombardier Rotax 914F engine in place of the earlier Limbach L2400. Most parts are made in Poland, but future production will be handled by Remos Aircraft. First seen at the 1996 Berlin Air Show, the S15 variant has a span reduced to 20.0 m (65 ft 7 in) and has two underwing hardpoints for scientific or surveillance sensor pods. There is also an unpiloted version, the S-UAV, again intended for surveillance. Variants S10 Standard production variant. S10V Variable pitch prop variant. S10VC Surveillance variant with underwing sensor pods. S10-VT 115hp Turbocharged Rotax 914F power. TG-11A S10s operated by the U.S. Air Force Academy Specifications below are for the S10-VT variant.
