Heinkel P.1080
| Industry | Aerospace, Defense |
|---|---|
| Founded | 1922 |
| Headquarters | Germany |
| Products | Aircraft |
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Template:Infobox aircraft
The Heinkel P.1080 was a conceptual fighter aircraft developed under the German Emergency Fighter Program by the manufacturer Heinkel.
Design and development
The P.1080 project commenced in early 1945 following directives from the Ministry of Aviation that outlined requirements for a fighter powered by a pair of ramjet engines. The design specified the use of two ramjets produced by the DFS, each delivering approximately 3,440 pounds (1,560 kg) of thrust.[1] The aircraft featured a tailless configuration, incorporating elevators within its swept wings—a design derived from the earlier Heinkel P.1078. It was equipped with a single vertical fin for stability. Positioned well forward in the fuselage was the cockpit, while the two ramjet engines were installed at the roots of the wings. The nose section was intended to house radar equipment alongside two 30 mm MK 108 cannon. For takeoff assistance, solid-fuel RATO units would have been attached, complemented by jettisonable landing gear. Upon landing, a retractable skid was planned to be used instead of conventional wheels. No actual prototypes were constructed.[1]
Specifications (Heinkel P.1080, conceptual design)
{{Aircraft specs |ref=[1] |prime units?=met |genhide=
|crew=1 |capacity= |length m=8.2 |length ft=26.8 |length in= |length note= |span m=8.9 |span ft=29.3 |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm=20 |wing area sqft=215.2 |wing area note= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= |eng1 number=2 |eng1 name=DFS |eng1 type=ramjet engine |eng1 kn=15.3 |eng1 lbf=3440 |eng1 note= |power original= |thrust original=
|eng2 number=4 |eng2 name=Solid-Fuel |eng2 type=RATO Boosters |eng2 kn=9.8 |eng2 lbf=2205 |eng2 note= |perfhide=
|max speed kmh=1000 |max speed mph=621 |max speed kts= |max speed note= |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= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |min control speed kmh= |min control speed mph= |min control speed kts= |min 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= |climb rate ms= |climb rate ftmin= |climb rate note= |max time to altitude s = |max time to altitude min = |max time to altitude note = |max time to altitude = |max time to altitude value = |max time to altitude unit = |max time to altitude reference = |max time to altitude source = |max time to altitude date = |max time to altitude comment = | | | | | | | | | | | | | | | | | | | | | | | | | | | | |
|max time to altitude = |max time to altitude value = |max time to altitude unit = |max time to altitude reference = |max time to altitude source = |max time to altitude date = |max time to altitude comment =
|max climb rate ms =
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|max climb rate ms =
|max climb rate ftmin =
|max climb rate note =