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MiG-21 FISHBED
J-7 (Jianjiji-7) / F-7
YF-110

The MiG-21F is a short-range day fighter-interceptor and the first major production version of the popular MiG-21 series. It is but one of many versions of this aircraft that have served in the air arms of many nations around the world. The E-5 prototype of the MiG-21 was first flown in 1955 and made its first public appearance during the Soviet Aviation Day display at Moscow's Tushino Airport in June 1956. During the Vietnam War, MiG-21s were often used against U.S. aircraft. Between April 26, 165, and January 8, 1973, USAF F-4s and B-52s downed 68 MiG-21s. More than 30 countries of the world-including nations friendly to the U.S. -have flown the MiG-21. At least 15 versions of the MiG-21 have been produced, some outside the Soviet Union. Estimates place the number built at more than 8,000, a production total exceeding that of any other modern jet aircraft.

The Soviets licenced the manufacture of the MiG-21F and its engine to China in 1961, and assembly of the first J-7 (Jianjiji-7 Fighter aircraft 7) using Chinese-made components began early 1964. The first flight of the Shenyang-built J-7 came on 17 January 1966, and Chengdu production of the J-7-I began in June 1967. Neither version was produced in large numbers. Subsequent modifications included development of the J-7-II / J-7B which began in 1975 with production approved in September 1979. Development of F-7M and J-7 III started in 1981. The J-7 III is the Chinese equivalent of MiG-21MF. Substantially reworked from the J-7 II, the J-7 III first flight occured on 26 April 1984. Jointly developed by Chengdu and Guizhou (GAIC), the J-7 III entered PLA Air Force and Navy service beginning in 1992, with production continuing thereafter.

Other development efforts extended through the F-7M Airguard which received a production go-ahead in December 1984. In 1988 China delivered the first 20 of 60 F-7M Skybolts to Pakistan. As upgrades, Karachi reportedly was leaning to a totally indigenous Chinese aircraft over the Grumman-influenced Sabre II, or F-7P. Development of the "Super 7" upgrade was terminated with the end of American technical assistance following the Tienanmen repression of 1989.

The aircraft has mid-mounted delta wings with small square tips. There is one turbojet inside the body. There is a small round air intake in the nose. There is a single exhaust. The fuselage is a long, tubular body with a blunt nose and bubble canopy. There is one belly fin under the rear section. There is a large dorsal spine flush with the canopy. The tail fin swept-back and tapered with a square tip. The flats are mid-mounted on the body, swept-back, and tapered with square tips. The J-7FS modification adds a radar to a reconfigured air intake, while the "Super 7" upgrade would have completely reworked the front end of the aircraft, adding a much larger radar and ventral air inlets, along with various other less pronounced improvements.

By 1989 Chinese production was running at a rate of as much as 14 aircraft per month, primarily for export. The J-7 aircraft was the most widely produced Chinese fighter, replacing older J-6 fighters, the Chinese version of the MiG-19. In 1995 it was projected that J-7 production would continue for at least another decade, resulting in a total inventory of nearly 1000 aircraft by 2005, but in fact the PLAAF inventory has remained static since then at about 500 aircraft, suggesting that production has either been suspended or terminated.

MiG-21 aircraft acquired by the United States under the Foreign Materiel Acquisition/Exploitation program are designated as the YF-110.
 
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Specifications
Countries of Origin Russia / China
Builder Mikoyan-Gurevich [Russia]
Xian Aircraft [China] @ Shenyang, Chengdu & Guizhou
Variants [td]MiG-21F Fishbed C MiG-21PF Fishbed D MiG-21PFM Fishbed F MiG-21R Fishbed H MiG-21S Fishbed H MiG-21RF Fishbed H MiG-21SM Fishbed J MiG-21M (Type 96/Hindustan Aeronautics-India) MiG-21PFMA Fishbed J MiG-21MF Fishbed J MiG-21SMT Fishbed K MiG-21SMB Fishbed K MiG-21bis-A Fishbed L MiG-21bis-B Fishbed N MiG-21U Mongol A MiG-21US Mongol B MiG-21UM Mongol B J-7 / F-7 Fishbed J-7 II / F-7B Fishbed J-7 III Fishbed F-7M Airguard F-7P Skybolt
Similar AircraftFitters, all models, Mirage III/5, A-4 Skyhawk
Role Ground-attack interceptor, trainer
Span23 ft. 6 in.
Length51 ft. 9 in.
Height15 ft. 9 in.
Weight18,080 lbs. max.
EnginesMiG-21 = Tumansky R-11F-300 @ 12,675 lbst w/afterburner
J-7 III = Wopen-13 turbofan @ 14,550-lbst
CrewOne
Maximum speed1,300 mph.
Cruising speed550 mph.
RangeMIG-21 = 400 mi range
MIG-21bis = 600 nm range
J-7 = 230 mi / 370 km lo-lo-lo radius
J-7B = 375 mi / 600 km radius w/ 2 PL-2 AAM + internal fuel
J-7B = 450 mi / 750 km radius w/ 2 PL-2 AAM + drop tanks
J-7M = 550 mi / 875 km radius w/ 2 PL-2 AAM + drop tanks
J-7 III = 525 mi / 850 km radius hi-hi-hi air superiority w/ 2 AAM + drop tanks
J-7 III = 340 mi / 550 km radius lo-lo-hi ground attack w/ 2 bombs + drop tanks
J-7 III = 1,350 mi / 2,200 km ferry range
 

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Service Ceiling 50,000 ft / 14000 meters  
Internal Fuel 2277 kg MIG-21pfs
2364 kg MIG-21bis
869 kg J-8  
In-Flight Refueling No
Drop Tanks MIG-21bis = Drop tank with 391kg of fuel for 51nm range
MIG-21bis = Drop tank with 631kg of fuel for 80nm range
MIG-21bis = Drop tank with 391kg of fuel for 50nm range
J-7 = 800 l drop tank with 639kg of fuel for 111nm range
Take-Off Runway F-7M = 700-950 m (2,300-3,120 ft)
J-7 III = 800 m (2,625 ft) with afterburning  
Landing Runway F-7M = 600-900 m (1,970-2,955 ft) with brake-chute
J-7 III = 550 m (1,805 ft) with flap blowing, drag-chute and brakes  
Sensors MIG-21pfs = Spin Scan (R1L) radar, RWR, Balistic bombsight MIG-21bis = Jay Bird radar, RWR, Balistic bombsight
J-7 = Type 222 ranging radar, RWR, Ballistic bombsight
Armament One NR-30 30mm cannon plus
MIG-21pfs = K-13 AA-2 atoll, FAB-500, FAB-250, UV-16-67 rocket pods
MIG-21bis = UV-69 57 rocket pods, AA-8 Aphid, FAB-250, FAB-500
J-7 = 2 PL-2 or PL-7 AAM and 1 800 L drop tank (685 nm)  
User Countries Afghanistan
Albania (J-7)
Algeria
Angola
Azerbiajan
Bangladesh
Bulgaria
Burma
Cambodia
China (J-7)
Congo
Croatia
Cuba
Czech Republic
Republic
Egypt
Ethiopia
Finland
Germany
Gunea
Hungary
India
Iran
Iraq
Kazakhstan
Laos
Libya
Madagascar
Mali
Mongolia
Mozambique
Nigeria
North Korea
North Yemen
Pakistan (J-7)
Poland
Romania
Slovakia
South Yemen
Sri Lanka
Sudan
Syria
Tanzania
Vietnam
Yugoslavia
Zambia
Zimbebwe





VRML 3-D Model

Mig-21 Fishbed
VRML by Soji Yamakawa
 

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J-7 (Jianjiji-7 Fighter aircraft 7) / F-7  

















 

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F-7FS




F-7P Sabre II "Super 7"


文章來自 :蘇聯與中國戰鬥機
 

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俄羅斯米格飛機公司


MiG-21 Fishbed 魚床


性能諸元如下:
全長:15.60m
翼展:7.15m
全高:4.50m
翼面積:23.0平方公尺
最大平飛速度:2.15Mach
最大起飛重量:10000kg
發動機型號:R-25-300渦扇噴射發動機
軍用推力:5400kg
後燃推力:7250kg
最大外載重量:1000kg
固定武裝:GSh-23 23mm機砲*2


發展沿革:
1950年代初期,前蘇聯空軍需要一種高速戰機,以擊落入侵敵機,爭取空優,所以發展出MiG-21戰機,由於設計時特別強調空戰及高速性能的發揮,所以簡省的許多非常必要性的裝備及油料,使航程縮短,而成為一種短程攔截機種,功能也受到一定的限制;然而其優異的空戰性能,卻是當時同期發展的戰機所難以比擬的。MiG-21首次出現在1956年6月的蘇聯航空展會場上空,北大西洋公約組織所給予的代號為「魚床」(Fishbed)。


MiG-21F 魚床C
為第一種量產型,航電系統相當簡陋,只具日間作戰功能。動力來源為1具圖曼斯基(Tumansky)的R-11F渦輪噴射發動機,軍用推力為4320kg,後燃推力為5760kg,使MiG-21可以達到2倍音速。

MiG-21PF 魚床D
為第2代生產型,具全天候作戰功能。機鼻進氣口及進氣錐予以加大,換裝較大型的R1L搜索/追蹤雷達,並將原有機砲拆除,只裝飛彈攻擊敵機。換裝R-11-F2S推力增為5960kg。加裝部分航電系統,並增加機內油量。


MiG-21PFS/PE 魚床E
換裝R-11-300發動機,最大推力6200kg;機腹下方加裝2具助升火箭,另增加一套吹翼系統(SPS),以縮短起降距離;換裝功能較為簡單的R2L雷達,可鎖定13Km內的目標。

MiG-21PFM 魚床F
由於原本的座艙罩掩蓋彈射式系統,卻因為構造複雜,反而容易造成彈射失敗,因此將其取消;並將原來整片式前開艙罩,分為風擋及右開艙蓋2部分;並改裝新式彈射椅。

MiG-21PFMA 魚床J
為第三代生產型,換裝新式雷達及射控系統,翼下可掛載4枚K-13A空對空飛彈或S-24空對地飛彈,和各類炸彈、火箭夾艙。
MiG-21MF 魚床J

換裝1具R-13-300渦輪噴射發動機,軍用推力5110kg,後燃推力可達6600kg,武裝配備與後期生產的MiG-21PFMA相同。
MiG-21R/RF 魚床H

為MiG-21系列的偵查機種,機上沒有武裝,機腹下方可掛偵查夾艙,內含紅外線偵側器、偵照相機及電子反制裝備;翼下掛架可掛載其他的偵察設備及副油箱。

MiG-21SMT 魚床K
為MiG-21MF改良型,武裝與其相同,但在翼下掛架可掛載電子反制夾艙,並改良機上射控系統及加大機內燃油裝載量。

MiG-21bis 魚床L

為第4代生產型,可擔任空戰及對地攻擊任務。機背予以加大加寬,以容納更多的電子設備;機內燃油容量增加至2300kg。

MiG-21bis 魚床N

為MiG-21bis後期生產型,改用1具R-25發動機,最大推力可達到7515kg。並改良航電系統,加裝抬頭顯示器,其雷達偵側距離為32Km,並可以改掛載R-60紅外線空對空飛彈。

MiG-21-93
換裝探測距離達57km的Kopyo雷達,具備發射R-77射後不理飛彈的能力,可視距外作戰。

MiG-21U/US/UM 蒙古A/B/B
為縱列雙座戰鬥教練機型,分別衍生自MiG-21PF/PFS/MF等單座戰鬥機。
 

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殲-7型戰鬥機

殲-7E的主要改進方面有:將三角翼該為雙三角翼,並裝有前後緣機動襟翼,這一設計為國內首創;增加發動機推力,降低油耗,將原噴7乙發動機換為渦噴13F發動機;加裝了平顯武器瞄準系統,大氣數據電腦等;換裝了航姿系統,無天線羅盤,信標接收機,無線電高度表,超短波電臺等;加挂高性能空空導彈;增加武器外挂能力,在機翼兩端各加一個外挂點,增強了空對地火力;增加了壓力加油系統,液壓系統採用密閉加油,以及對平尾和副翼載荷進行設計改進等。改進後的飛機其低空格鬥能力,起降性能,對地火力,續航時間都有了顯著的提高,並對未來電子戰有一定的適應能力。

從殲-7E的改進改型來看,該機最突出的改進是近距格鬥能力的大幅提升。提高穩定盤旋角速度要受三個條件的限制:一是最大載荷限制,一般不超過8-9個g;二是失速限制,要求儘量提高Cy,並儘量降低翼載荷;三是可用推力的限制,要求儘量提升推重比。由於殲-7E將原三角翼改為雙三角翼,並安裝了前後緣機動襟翼,使該機的Cy大幅提升;別外,由於換裝了WP-13F發動機(發動機推力6560kg)可用推力增加460kg,這些都對穩定盤旋性能的提升起到了良好的作用,同時由於PW-13系列發動機中更大推重比的新機型已批量生產,殲-7E的機動性能還有進一步提升的餘地,改進後的殲-7E在中低空穩定盤旋性能與F-16A基本相當,這對於持續空中格鬥尤為重要。

水準機動性能的另一項重要指標是暫態盤旋性能,通常是以減速來達到,因此不受可用推力限制,只受承載能力和失速限制。由於殲-7E的翼載荷較小,因此,殲-7E在暫態機動性上佔有優勢。殲-7E由於Cy大幅提升,翼載荷也有一定程度的下降,估計該機的失速表速將會比殲-7II的210-220km/s 有較大程度的放寬,這無疑將對提升殲-7E的暫態盤旋性能起到重要作用。

殲七的最新改進型就是殲-7FS,從外形上看,殲-7FS與原有殲-7系列戰鬥機的最大區別是,改變了原機頭進氣方式,即演變為下頜式進氣,這種進氣方式與美國的A-7“海盜”攻擊機類似。這種改進有兩個優點:首先增加了機鼻的容積,便於安裝大功率的機載雷達;其次,提高了大仰角飛行時的進氣效率,從而使飛機的姿態機動能力增強。

原來的殲-7系列戰鬥機的機載雷達只能裝在直徑狹小的進氣口整流錐內,雷達掃描天線的大小受到嚴格限制(若太大會造成進氣量減小,無法滿足發動機的正常工作要求),所以僅裝備小功率的測距雷達,如GEC-馬可尼公司的“空中巡邏兵”226型火控雷達。它的作用距離基本在20千米左右,而且只能跟蹤/攻擊單一目標,無法賦予戰鬥機進行視距外空戰能力,從而影響作戰效能的發揮。殲-7FS通過上述巧妙改進之後,雷達艙允許裝置的雷達掃描天線直徑超過了600毫米。完全可以選用類似于俄羅斯“甲蟲”系列的先進火控雷達作為標準裝備。“甲蟲”雷達為多功能脈衝多普勒雷達,可以制導多種導彈,其對雷達反射截面為3平方米的目標的搜索/跟蹤距離,前半球超過70千米,後半球為40千米。它還具有上視、下視能力,可以同時跟蹤10個目標,並能引導中距空空導彈同時攻擊其中的2個目標,這賦予了殲-7FS視距外空戰能力。

此外,為了進一步改善動力性能,殲-7FS換裝了渦噴-13F II(WP-13F II)型發動機。這種發動機是黎陽發動機公司在原殲-8 II型戰鬥機上裝載的渦噴-13(WP-13)型發動機的基礎上改進而來的。推力進一步增加到78千牛(約8000千克),這使得殲-7FS的機動能力較原殲-7系列戰鬥機有了大幅提高。如最大爬升率從139米/秒增加到199.8米/秒;在5000米高度,從0.6馬赫加速到1馬赫的時間由35秒減少到28.7秒;起飛滑跑距離也縮短了200米等等。

殲-7FS還將逐步改善其機載電子設備,計劃更換雷達冷卻系統、電路系統、飛行參數記錄系統、武器管理系統、GPS導航系統和多功能座艙顯示器。並準備將機翼修改為與殲-7MG相同的“雙三角翼”,以進一步提高其近距格鬥時的機敏性。
 

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在台灣也有一架,是中共孫天勤義士於民國72年8月7日自遼東半島[三十里堡]機場駕機起義降落韓國城南(K-16)基地(現仍停放韓境)同一機型,現放置於岡山的空軍官校的軍機展示場



[ 本文最後由 勛老大 於 07-2-11 02:47 PM 編輯 ]
 
騎白馬的不一定是王子 也有可能是唐僧
打手槍的不一定是變態 也有可能是九把刀

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克里斯Chris    發表於 07-2-11 16:14 聲望 + 1 枚  回覆一般留言
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