- Design and development
- Variant
- Specifications
- References
- External links
name=Stemme ASP S15 | image=File:Safran Electronics & Defense Patroller.jpg | caption=A SAGEM Patroller, UAV variant of the ASP S15 }}{{Infobox Aircraft Type | type= Motor glider | national origin=Germany | manufacturer=Stemme | designer= | first flight= | introduced= | retired= | status= | primary user= | number built= | developed from= | variants with their own articles= SAGEM Patroller }} |
The Stemme ASP S15 is a German two-seat powered sailplane designed and built by Stemme for use as an Airborne Systems Platform. Design and developmentThe ASP S15 is a two-seat single-engined, all composite construction, powered sailplane with the engine mounted in the center fuselage. The cockpit has room for two in side-by-side configuration.[1] It has a shoulder wing, a conventional T-tail and a retractable nose wheel landing gear.[1] It can also be fitted with a 2-axis autopilot and external underwing payload pods.[1] The ASP S15-1 was granted a restricted type certificate by the European Aviation Safety Agency in October 2013.[1] Variant- ASP S15-1
Airborne Systems Platform which can be fitted with a 2-axis autopilot and external underwing payload pods.[1] - //SAGEM Patroller">SAGEM Patroller
An unmanned variant in partnership with the French company SAGEM. Specifications{{Aircraft specs |ref=[1] |prime units?=met |genhide= |crew=2 |capacity= |length m=8.52 |length ft= |length in= |length note= |span m=18 |span ft= |span in= |span note= |height m=2.45 |height ft= |height in= |height note= |wing area sqm=17.4 |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=1100 |max takeoff weight lb= |max takeoff weight note= |lift note= |more general=
|eng1 number=1 |eng1 name=Rotax 914 F2 |eng1 type= |eng1 kw=84.5 |eng1 hp= |eng1 kn= |eng1 lbf= |eng1 note= |prop blade number=3 |prop name=Mühlbauer Type MTV-7-A / 170/051 |prop dia m=1.7 |prop dia ft= |prop dia in= |prop note=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh=265 |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |power/mass met= |power/mass imp= |power/mass note= |thrust/weight= |thrust/weight note= |more performance= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
References1. ^1 2 3 4 5 EASA Type Certificate Data Sheet Stemme ASP S15-1
External links{{commons category|Stemme}}- {{Official website|http://www.ecarys.com/stemme-ums/}}
{{Stemme aircraft}} 4 : Stemme aircraft|Motor gliders|German civil utility aircraft 2000–2009|Shoulder-wing aircraft |