请输入您要查询的百科知识:

 

词条 Gribovsky G-28
释义

  1. Design and development

  2. Specifications

  3. References

name=Gribovsky G-28 image= caption=

}}{{Infobox Aircraft Type

type=Advanced trainer national origin=USSR manufacturer= designer=Vladislav Gribovsky first flight=22 May 1941 introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Gribovsky G-28 ({{lang-ru|Грибовский Г-28}}, VVS designation TI-28) was an advanced trainer for trainee fighter pilots, built in the USSR just before the German invasion in 1941. It satisfied VVS testing but changing priorities led to the abandonment of production plans.

Design and development

The TI in the VVS name for the G-28 indicated its function as a Trenirovochni Istrebitel or Fighter Trainer. After basic training a prospective fighter pilot could gain experience of the characteristics of a quite fast, manoeuvrable, single seat, enclosed cockpit aircraft, fitted with guns or bombs. It was, like all earlier Gribovsky aircraft, almost entirely of wooden construction.

Its cantilever low wing had two wooden spars and was plywood skinned. The ailerons were fabric covered duralumin frames and the inboard, pneumatically activated flaps were also duralumin. In plan the wing was strongly tapered, mostly on the trailing edge, carefully faired into the fuselage at the wing roots and ending in elliptical tips.

The G-28 was powered by a {{convert|270|hp|kW|abbr=on|0|order=flip}} MV-6 six cylinder inverted in-line engine, driving a two blade variable pitch propeller. The engine was on a steel tube mounting and enclosed in a light-alloy cowling. The fuselage was a wooden monocoque with an integral fin. A cockpit with a sliding, multi-panel canopy was situated over the trailing wing root, merging into the raised upper rear fuselage behind it. At the rear the tailplane was mounted on the upper fuselage. Both elevators and the rudder were aerodynamically balanced, fabric covered dural structures. In plan the horizontal tail was elliptical, with a small cut out for movement of the curved rudder, which extended down to the keel.

Though the G-28 had some of the characteristics of contemporary fighters, it differed in having a fixed tailwheel undercarriage. Each unfaired main wheel was on a cantilever oleo leg from the forward spar; the tailwheel castored. Its armament was simple, with a single machine gun aimed with a reflector sight and monitored with a wing root camera. A pair of underwing racks could each carry two bombs with weights up to {{convert|40|kg|lb|abbr=on|0}}.

The G-28 first flew on 22 May 1941. It was flight tested by the VVS and found satisfactory, though Gribovsky hoped to install the more powerful MV-6A engine variant in production aircraft. After the German invasion of the USSR in June 1941, Gribovsky's priority became production of the Gribovsky G-11 assault glider and the G-28 was abandoned.

Specifications

{{Aircraft specs
|ref=Gunston (1995) pp.81-2
|prime units?=met


|genhide=
|crew=One
|length m=7.66
|length note=
|span m=9.0
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=11.6
|wing area note=
|aspect ratio=
|airfoil=RAF 34
|empty weight kg=897
|empty weight note=
|gross weight kg=1157
|gross weight note=without bombs
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=MV-6
|eng1 type=6-cylinder inverted air-cooled piston engine
|eng1 hp=270
|eng1 note=[7]
|more power=
|prop blade number=2
|prop name=Ratier
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=ariable pitch


|perfhide=
|max speed kmh=303
|max speed note=at {{convert|1600|m|ft|abbr=on}}; {{convert|275|km/h|mph kn|abbr=on|0}} at sea level
|cruise speed kmh=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=500
|range note=at 90% of maximum speed
|ceiling m=6600
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=19.4 min to {{convert|5000|m|ft|abbr=on}}
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=

  • Landing speed: {{convert|90.5|km/h|mph|abbr=on|0}} with flaps

}}

References

1. ^{{cite book |title= The Osprey Encyclopedia of Russian Aircraft 1875-1995|last=Gunston|year=1995|page=XXI}}
[1]
}}{{Gribovsky aircraft}}

4 : Soviet military trainer aircraft 1940–1949|Gribovsky aircraft|Low-wing aircraft|Aircraft first flown in 1941

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/11 14:07:28