Grigorovich IP-1

{{Infobox Aircraft Begin

| name = IP-1, IP-4

| image = Grigorovich IP-1.jpg

| caption =

}}{{Infobox Aircraft Type

| type = Fighter

| national origin = Soviet Union

| manufacturer = Grigorovich, GAS № 135

| designer = Dmitry Grigorovich (engineer)

| first flight = 1935

| introduced = 1936

| retired = 1940

| status =

| primary user = Soviet Air Force

| more users =

| produced =

| number built = ca. 90

| variants with their own articles =

}}

The Grigorovich IP-1 (for Истребитель Пушечный - "Cannon fighter") was a fighter aircraft produced in the Soviet Union in the 1930s by the Grigorovich Design Bureau.{{cite magazine |author= |title=A-Z of Aircraft Files #895, Sheet 12 |url= |magazine=World Aircraft Information Files |location=United Kingdom |publisher= Bright Star Publications |date= |access-date=}}

The IP-1 started development as the GD-52 in 1934. An all-metal aircraft, it featured an open cockpit, retractable wing wheels, an advanced, nearly-elliptical cantilever wing, and a variable-pitch, metal propeller powered by a 640 hp (477 kW) Wright Cyclone series engine. Retractable skis could be fitted for winter use, a first for any Soviet aircraft. The DG-52 was transferred to the Air Force Research Institute on 12 January, 1935 for testing, and was flown that same day by P.Ya. Fedrovi.https://war-book.ru/grigorovich-ip-1-istrebitel/ {{Bare URL inline|date=August 2024}}{{rs|date=June 2024}}{{cite web | url=http://aviadejavu.ru/Site/Crafts/Craft32014.htm | title=Григорович ИП-1 / ИП-4 }}{{rs|date=June 2024}}{{Cite web|url=http://авиару.рф/aviamuseum/aviatsiya/sssr/istrebiteli-2/1920-e-1930-e-gody/pushechnye-istrebiteli-ip/pushechnyj-istrebitel-ip-1-dg-52/|title=Пушечный истребитель ИП-1 (ДГ-52). - Российская авиация}}{{rs|date=June 2024}}

Like the preceding Grigorovich I-Z, the IP-1 prototype was built around the cannon-fighter concept, with two Leonid Kurchevsky-designed APK-4 76.2mm cannons mounted under the wings, each capable of 5 shots before ammunition was depleted. It was also armed with two 7.62mm machine guns. Production aircraft used the licensed copy of the Wright Cyclone, the Shvetsov M-25. After 90 aircraft had been produced and 30 delivered, it became apparent that there were issues with lateral stability and especially spin. On 3 June, 1936 Lieutenant Bolshakov of the 92nd Air Brigade fell into a flat tailspin at 1,700m, and had to bail out with a parachute. This led to further refinements to the structure. On 3 May 1936 it was decided to replace the APK-4 cannons with two 20mm ShVAK cannons. Six 7.62mm ShKAS machine guns were installed, three in each wing. 200 units were produced from 1936 to 1937, but the IP-1 was soon overshadowed by the Polikarpov I-16.{{rs|date=June 2024}}{{rs|date=June 2024}}{{cite web | url=https://allaircraft.ru/146-grigorovich-ip-1.html | title=Григорович ИП-1 }}{{rs|date=June 2024}}

On 1 February, 1940 six IP-1s were in service at the ShMAS Air Force in the Moscow Military District, and eight at the Air Force Control Center, though the latter had been dismantled for use as spare parts. In October 1940 the 21 remaining aircraft were written off as unusable.{{rs|date=June 2024}}

Variants

In 1939 it was proposed to utilize the IP-1 as an attack aircraft rather than a fighter. IP-1 number 135 was armed with Six ShKAS machine guns, and 6-6.5mm armor was added to the gas tanks, cockpit, and engine. Seven more aircraft were also converted to the new attack configuration, and these were designated IP-1sh. Flight tests were carried out on 5 & 6 June, 1939, where it was determined that the tendency to spin was too great and the project was abandoned. One IP-1sh was sent to NKSP Research Institute 48 to be used as a target for determining armor effectiveness.{{rs|date=June 2024}}

An IP-1 fitted with a 690 hp (514 kW) Hispano-Suiza 12Xbrs engine was given the designation IP-2 (DG-54). Armed with an engine-mounted ShVAK cannon and 10 ShKAS machine guns, the prototype was nearly complete when abandoned in 1936.{{rs|date=June 2024}}

The IP-4 (DG-53) fighter was designed in 1934. Armament consisted of four 45mm Kurchevsy APK cannons and two machine guns. A second prototype (DG-52bis) with ShVAK cannon replacing the Kurchevsy weapons was designed but never built.{{rs|date=June 2024}}

The armament of the IP-4 consisted of four fixed dynamo-reactive 45-mm L.V. guns. Kurchevsky ARK-11 and two rifle-caliber machine guns. Like the IP-1 prototype, the IP-4 fighter prototype was equipped with a Cyclone engine. A second prototype with two ShVAK guns instead of the Kurchevsky guns was designed, but not built.

Operators

;{{USSR}}

Specifications (IP-1)

{{Aircraft specs

|prime units? = met

|crew=One pilot

|length m=7.23

|length ft=23

|length in=9

|span m=10.97

|span ft=36

|span in=0

|wing area sqm=20.0

|wing area sqft=215

|empty weight kg=1,200

|empty weight lb=2,646

|gross weight kg=1,880

|gross weight lb=4,145

|eng1 number=1

|eng1 name=Shvetsov M-25

|eng1 kw=530

|eng1 hp=710

|max speed kmh=410

|max speed mph=255

|range km=600

|range miles=373

|ceiling m=8,300

|ceiling ft=27,230

|climb rate ms=12.8

|climb rate ftmin=2,520

|armament = *2 × fixed, forward-firing 7.62 mm ShKAS machine guns in forward fuselage

  • 2 × fixed, forward-firing 20 mm ShVAK cannons in wing roots
  • 6 × fixed, forward-firing 7.62 mm ShKAS machine guns in trays under wings

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

{{reflist}}

{{commons category|Grigorovich IP-1}}

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=441 }}
  • {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 895 Sheet 12–13 }}

{{Grigorovich aircraft}}

{{Soviet fighter designations}}

Category:1930s Soviet fighter aircraft

Category:Grigorovich aircraft

Category:Single-engined tractor aircraft

Category:Low-wing aircraft

Category:Aircraft first flown in 1935

Category:Aircraft with retractable conventional landing gear

Category:Single-engined piston aircraft