convair King fish
Aircraft
The Convair Kingfish reconnaissance aircraft design was the ultimate result of a series of proposals designed at Convair as a replacement for the Lockheed U-2. Kingfish competed with the Lockheed A-12 for the Project Oxcart mission, and lost to that design in 1959.
King fish
After cancellation of the B-58B in mid-1959, Convair turned to a completely new design, similar to their earlier entry in name only. The new "Kingfish" design had much in common with the Convair F-106 Delta Dart, using a classic delta wing layout like most of Convair's products. It differed in having two of the J58 engines buried in the rear fuselage, and twin vertical surfaces at the rear. The intakes and exhausts were arranged to reduce radar cross section, and the entire aircraft had the same sort of angular appearance as the later Lockheed F-117. The leading edges of the wings and intakes continued to use pyroceram, while other sections used a variety of materials selected for low radar reflection, including fiberglass. The new engines reduced the cruise speed to Mach 3.2, compared to Mach 4.2 for the FISH, but range was increased to about 3,400 nm (6,300 km).
In July 1959, Lockheed and Convair presented preliminary designs and cross selection estimates to the review panel. Lockheed's was designated the A-12, and was a variation of their A-11 design. President Eisenhower was briefed on 20 July and he approved moving ahead with a final decision. On 20 August, the companies presented their final designs for Kingfish and the A-12. Lockheed's design was estimated to have longer range, higher altitude and lower cost.[5] Johnson expressed skepticism of Convair's claimed RCS, and complained that they had given up performance to achieve it: "Convair have promised reduced radar cross section on an airplane the size of A-12. They are doing this, in my view, with total disregard for aerodynamics, inlet and afterburner performance."
On 28 August 1959, Johnson was notified that the A-12 had been selected. The decision was based not only on aircraft performance but also on contractor performance. During the U-2 project, Lockheed had proven its ability to design advanced aircraft in secret, on-time, and under-budget. In contrast, Convair had massive cost overruns with the B-58 and no secure R&D facility similar to the Skunk Works. Lockheed promised to lower the RCS in a modified version of the A-11 known as the A-12, and that sealed the deal. The A-12 entered service with the CIA in the 1960s, and was slightly modified to become the Air Force's SR-71.
Specifications
General Characteristics
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- Wingspan 38.3ft (11.7m)
- Length 45.1ft (13.8m)
- Height 11.6ft (3.5m)
- Empty Weight 20,717lbs (9,397kg)
- Loaded Weight 33,600lbs (15,240kg)
Performance
- Power/Weight Ratio 1.337
- Wing Loading 36.7lbs/ft2 (179.2kg/m2)
- Wing Area 915.6ft2 (85.1m2)
- Drag Points 4133
Parts
- Number of Parts 70
- Control Surfaces 8
- Performance Cost 422
@Pakdaaircraftindustries no problem :)
@CatdogAerospace thanks I will take this into account next time
@Pakdaaircraftindustries here are the rules the aircraft must be under 96 parts and can't have more than 7 wings
@CatdogAerospace there's a post explaining pea aircrafts?
There are 8 WINGS meaning this in no longer [PEA]