發信人: SAAF (武神 伐千秋)    看板：Aero
日期： Sat Apr 25 21:29:32 1998
標題： Re: Mig42


>Who has Mig42's file

1.42是米高揚設計局所設計的多功能前線戰機,還屬於實驗
機階段所以還未賦與正式編號..這款機型幾乎是集俄羅斯所
有高科技之大成,集一低視度,暱蹤,向量操作,...等未來戰
機的一切條件...以下是其簡介...

Mikoyan article 1.42 also known as MFI (Mnogofunktsionalny 
Frontovoi Istrebitel - Multifunctional Frontline Fighter), 
and sometimes referred to in the West as "ATFski" is a low-observable 
(LO) multirole fighter. The primary mission of the 1.42 is 
air-superiority as the primary mission, which makes 1.42 a direct
Russian equivalent of the USAF F-22. The chief designer of MiG
 MAPO Mr. Belosvet stated that 1.42 would have a greater range 
than the F-22 and would be more versatile. While F-22 primary task is
 achievement of the air superiority, the 1.42 will be as capable in 
strike mission as in air combat. The 1.42, like the F-22,can carry 
weapons both internally and externally, will be capable of supercruise
and powered by trust-vectored control (TVC) engines.

//The Powerplant//

Saturn-Lyulka was to develop an engine for the new
 fighter. This task turned out to be very demanding 
and Al-41F development experienced number of the setback 
stalling the whole 1.42 program. The new engine had a 
higher combustion chamber temperature -- 250 degrees
 than that of Su-27 Flanker's Al-31F -- which provided
an outstanding performance. Although the original plans
 called for a 2D F-22 style trust-vectoring nozzles, the
recent reports suggested that Al-41F TVC  was similar to
 Al-37FU powering the superagile Su-37. The secrecy and
controversy surrounded 1.42 and its engines produced 
many speculations about 1.42 TVC. The fuzziest comment 
was given in 1995 by RIA: "specially arranged nozzles to 
enable it [1.42] to hover over a target for pinpoint 
strike accuracy."

1.42 vital statistics

DIMENSIONS:
Wingspan                  similar to Su-27
Length overall            "
Height overall            "
WEIGHTS AND LOADINGS:       
Weight empty, equipped    NA
Max T-O weight            30,000-35,000 kg (20,745 lb)
Max landing weight        NA
Max wing loading          NA
Max power loading         NA
PERFORMANCE (estimated):                
Max level speed:    
at height                 NA
at S/L                    NA
T-O speed                 NA
Landing speed             NA
Service ceiling           NA
T-O run                   NA
Landing run               NA
Range with max fuel                    
at S/L                    NA
at height                 NA
G-limits                  NA
ARMAMENT:
                                          
Number of hardpoints:     12-14(?): some conformal
Air-to-air:               R-77, R-73, K-37, K-74 
Air-to-surface:           NA 




--
秋臨風起，葉飛此時，不是悲秋客，卻為落葉人。

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* Origin: 國立中山大學 Formosa BBS * From: 140.130.101.239 [已通過認證]
.