超级军网[讨论]FC－7同MIG－33的内在联系
来源：百度文库 编辑：超级军网 时间：2024/04/29 11:19:08
Initially it was anticipated（预期） that the Super-7/FC-1 would be a high-performance, low-cost fighter plane to replace outdated F-5s and MiG-21s in many third-world air forces. But with the participation of MASPG（米高扬）, the Russians are using the Super-7/FC-1 as a continuation（延续） of the MiG-33 (R33) programme developed in the 1980s. Like the MiG-33, the Super-7/FC-1 uses the RD-93 turbofans（扇涡轮）, though the Super-7/FC-1 features air inlets（进气口） on the lateral sides（侧面） of the fuselage（机身） rather than the ventral（腹部) inlets of the MiG-33. With Russian technical assistance the redesigned Super-7/FC-1 has improved climb out performance and steering capabilities along with a stronger fuselage.
However, the most apparent modifications（改动） to the MiG-33 design is the repositioning of the （ventral fins？？） from the engine compartment to the added （tail edgings？？）, providing aerial manoeuvrability（机动性） that is claimed to match that of the U.S. F-16. These improvements in performance have affected the programme's costs, and if the final production order is fewer than 300 aircraft the unit price will rise from the original $10 million to $15 million.
[em04][em04][em04][em04]Initially it was anticipated（预期） that the Super-7/FC-1 would be a high-performance, low-cost fighter plane to replace outdated F-5s and MiG-21s in many third-world air forces. But with the participation of MASPG（米高扬）, the Russians are using the Super-7/FC-1 as a continuation（延续） of the MiG-33 (R33) programme developed in the 1980s. Like the MiG-33, the Super-7/FC-1 uses the RD-93 turbofans（扇涡轮）, though the Super-7/FC-1 features air inlets（进气口） on the lateral sides（侧面） of the fuselage（机身） rather than the ventral（腹部) inlets of the MiG-33. With Russian technical assistance the redesigned Super-7/FC-1 has improved climb out performance and steering capabilities along with a stronger fuselage.
However, the most apparent modifications（改动） to the MiG-33 design is the repositioning of the （ventral fins？？） from the engine compartment to the added （tail edgings？？）, providing aerial manoeuvrability（机动性） that is claimed to match that of the U.S. F-16. These improvements in performance have affected the programme's costs, and if the final production order is fewer than 300 aircraft the unit price will rise from the original $10 million to $15 million.
[em04][em04][em04][em04]
However, the most apparent modifications（改动） to the MiG-33 design is the repositioning of the （ventral fins？？） from the engine compartment to the added （tail edgings？？）, providing aerial manoeuvrability（机动性） that is claimed to match that of the U.S. F-16. These improvements in performance have affected the programme's costs, and if the final production order is fewer than 300 aircraft the unit price will rise from the original $10 million to $15 million.
[em04][em04][em04][em04]Initially it was anticipated（预期） that the Super-7/FC-1 would be a high-performance, low-cost fighter plane to replace outdated F-5s and MiG-21s in many third-world air forces. But with the participation of MASPG（米高扬）, the Russians are using the Super-7/FC-1 as a continuation（延续） of the MiG-33 (R33) programme developed in the 1980s. Like the MiG-33, the Super-7/FC-1 uses the RD-93 turbofans（扇涡轮）, though the Super-7/FC-1 features air inlets（进气口） on the lateral sides（侧面） of the fuselage（机身） rather than the ventral（腹部) inlets of the MiG-33. With Russian technical assistance the redesigned Super-7/FC-1 has improved climb out performance and steering capabilities along with a stronger fuselage. However, the most apparent modifications（改动） to the MiG-33 design is the repositioning of the （ventral fins？？） from the engine compartment to the added （tail edgings？？）, providing aerial manoeuvrability（机动性） that is claimed to match that of the U.S. F-16. These improvements in performance have affected the programme's costs, and if the final production order is fewer than 300 aircraft the unit price will rise from the original $10 million to $15 million.
[em04][em04][em04][em04]打问号的地方，谁帮忙翻译一下。气动布局上的区别谁能拿张图来说明一下。