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Strategy for R&D: Studies in the Microeconomics of Development
註釋89 TABLE 5 USE OR PLANNED USE OF MAJOR ENGINES IN AIR FORCE AND NAVY AIRCRAFT a Engine Air Force Aircraft Navy Aircraft F-80, T-33, XF-92, YB-61, AJ2, F9F-7, TV-I, J-33 YB-62, F-94 (A, B), TM- T2-V, P4M-I 61 (tactical missile) X-3, XF-88 F3D, F2H, F6U, F7U J-34 F-84 (B, C, D, E, G, H) J-35 FJ-I B-45, XB-51, XF-9J, B-36, J-47 B-47, F-86 (D, F, K) J-48 F-94C F9F J-57 B-52, YB-60, F-lOO, A3D, F4D, F8U F-I02A, F-I0l (A, B), SNARK, F-105A, F-I07, KC-135A, B-57D, X-16 F-84F, B-57 FIIF, A4D, FJ-3, J-65 FJ-4, F9F YQ-l, YQ-2, T-37 J-69 SNARK, YF-89E, B-66 J-71 F-I01, F-I02B, F-I05, J-75 F-I07 F8U, XP6M B-58, F-I04, F-IOIA (see J-79 note c, Table 4) F5D, FIIF, A3J, F4H T-34 C-133A, YC-97J, YC-12IF R7V-2 XF-84H T-40 R3Y, XFY, A2D YC-130, YC-131C T-56 Note: a Aircraft in which engine was used or was planned to be used. For at least one (and generally more) of the aircraft in the list associated with a given engine, the decision to use the engine was made when the engine was in the final stages of developƯ ment. (In the case of the J -57, J-79, andJ-75 this is true of nearly all the aircraft listed.) No Jist extends beyond 1956. Summary For an engine developed independently of an airframe the deƯ veloper may constrain the performance, weight, and size of an engine at the start.