Складничок -2
1. Inboard profile drawing of AMSA Configuration 2906. AMSA, short for advanced manned strategic aircraft, was a precursor to what eventually led to the B-1 bomber. Drawing is dated 5 June 1967.



2. Drawing of AMSA Configuration 1315. AMSA, short for advanced manned strategic aircraft, was a precursor to what eventually led to the B-1 bomber. Drawing is dated 9 August 1967.



3. F-111D inboard profile. Drawing dated 6 May 1969.



4. Drawing of AMSA Configuration 1311. AMSA, short for advanced manned strategic aircraft, was a precursor to what eventually led to the B-1 bomber. Drawing is dated 17 August 1969.



5. Basic drawing for two-engine B-1. Drawing dated 16 January 1970.



6. Basic drawing for fixed-wing B-1. Drawing dated 16 January 1970.



7. Drawing of interioir arrangement of an airliner done as part of the Advanced Transport Technology Program for NASA. Drawing dated 5 March 1971.



8. Drawing of F-16 SCAMP Model 400-1. Dated September - December 1978. SCAMP stood for supersonic cruise and manuever prototype. The design led to the F-16XL.



9. Drawing of ATF Configuration 100 dated 28 January 1965.


10. Six-man crew module study for advanced manned strategic aircraft, or AMSA. This program was a precursor to what eventually led to the B-1 bomber. Drawing is dated March 1968.


11. General arrangement drawing of AMSA Configuration 2906. AMSA, short for advanced manned strategic aircraft, was a precursor to what eventually led to the B-1 bomber. Drawing is dated 6 March 1967.


12. Lockheed hypersonic transport design study CL-445-1 from the late 1950s. One of a series of drawings that show several aircraft configurations with takeoff gross weights up to 565,000 pounds, ranges of 4,000 nautical miles, and cruise speeds of Mach 5.


13. Lockheed studied an air-sea craft in the late 1960s. CL-936-2, shown here, was powered by four above-wing turbofan engines. The design weighed 270,000 pounds (gross weight).


14. CL-293 was Lockheed design (circa 1955) powered by six turbojet engines and one 320-megawatt nuclear reactor. The aircraft had a gross weight of 603,900 pounds.


15. CL-507 was a Lockheed preliminary design effort in 1960 that involved a series of STOVL and VTOL fighter bombers with maximum speeds in the Mach 2 range. This variation (507-27) had variable-sweep wings.


16. Lockheed studied vertical and short takeoff and landing transports for the US Marine Corps in the early 1960s. CL-484-5-4 design, shown here, had two turbofan engines for cruising and eight engines for vertical lift.


17. The Space Logistics, Maintenance and Repair, or SLOMAR study, was initiated by the USAF in 1959. The basic objectives of the SLOMAR study were to estimate future military space needs in terms of support for manned space stations and produce preliminary designs of vehicles to fulfill that mission. This concept was labeled CL-498. Click on the image above to see it in its entirety.


18. General arrangement drawing of AMSA Configuration 2906. AMSA, short for advanced manned strategic aircraft, was a precursor to what eventually led to the B-1 bomber. Drawing is dated 6 March 1967.