- Design and development
- Specifications
- See also
- References Note Bibliography
name=AG-1 | image= | caption= }}{{Infobox Aircraft Type | type=Assault glider | national origin=United States | manufacturer=Christopher Company | designer= | first flight= | introduced= | retired= | status=Project cancelled | produced= | primary user= | number built=None | developed from= | variants with their own articles= | developed into= }} |
The Christopher AG-1 was a proposed Second World War American assault glider part of a United States Army assault glider project, none were built and the programme was cancelled in September 1943. Design and developmentThe United States Army had an idea to procure an assault glider, an armed glider that would land first and help secure the landing site for the use by transport gliders. Each assault glider would have six glidermen as well as the pilot and co-pilot, the glidermen would be armed with two .50 and two .30 calibre machine guns and two rocket launchers. Contracts were awarded in May 1943 to two companies, the Christopher Company and the Timm Aircraft Company, each to build two prototypes. The Christopher prototype was designated the XAG-1 and was to have been a low-wing cantilever monoplane with a gross weight of 8500lb, the company delivered a wind tunnel model to the Army. General Chidlaw in the Office of the Assistant Chief of Air Staff decided that it was damned fool idea and cancelled the project in September 1943. Specifications {{Aircraft specs |ref=Mrazek |prime units?=imp |genhide= |crew=2 (pilot, co-pilot) |capacity=6 glidermen |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=8500 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |more general=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph=240 |cruise speed kts= |cruise speed note=while being towed |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |more performance= }}
See also{{aircontent |see also= |related= |similar aircraft= |lists= }}ReferencesNoteBibliography- {{cite book |last= Andrade |first= John |title= U.S.Military Aircraft Designations and Serials since 1909|year=1979 |publisher=Midland Counties Publications|isbn=978-0-904597-22-6}}
- {{cite book|first=James E.|last=Mrazek|title=Airborne Combat - The Glider War/Fighting Gliders of WWII|publisher=Stackpole Books|year=2011|location=Mechanicsburg, Pennsylvania, United States|isbn=978-0-8117-0808-1}}
{{USAAF glider aircraft}} 2 : United States attack aircraft 1940–1949|United States military gliders 1940–1949 |