Pashinin I-21

The Pashinin I-21 (not to be confused with the Ilyushin TsKB-32, also known as "I-21") was an early 1940s Soviet fighter prototype. Designed by Mikhail M. Pashinin, the I-21 was built to incorporate lessons learned from the combat experiences of Soviet pilots during the Spanish Civil War and the Nomonhan Incident with the Empire of Japan. Despite showing promising performance, the I-21 did not get past the prototype stage, as it was felt the type did not offer a significant enough increase in capability over competitors already in production, such as the Yakovlev Yak-1 or Mikoyan Gurevich MiG-3.

Development

Mikhail Pashinin began development of his monoplane fighter in early 1939. A former employee of N. N. Polikarpov, Pashinin envisioned the I-21 as a replacement for the increasingly obsolescent I-16 in Soviet service. The resulting I-21 featured a low set wing with retractable undercarriage, a Klimov M-107 engine, and a framed canopy with good visibility. The I-21 was of mixed construction, as typical of many contemporary designs, and had a monocoque rear fuselage made of wood, whereas the forward fuselage was built from welded steel tubing for increased rigidity. Wings were of metal with plywood covering.

The cockpit was placed well aft, behind the wing, and the pilot was seated under a swinging canopy. The I-21's armament consisted of an engine mounted 20 millimeter ShVAK automatic cannon and two 7.62 millimeter ShKAS machine guns, one in each wing. This armament was typical of other Soviet fighters of the period such as the Yak-1. The 20mm ShVAK was later replaced by a harder-hitting 23mm BT-23 cannon.

The prototypes were ultimately powered by Klimov M-105P engines, since the M-107 had run into development troubles of its own, and production of the engine was delayed. Flight testing with the 1,050-hp M-105 began with the first flight on 18 May 1940. Official testing by Soviet authorities was conducted from 6 June, in test pilots discovered that the I-21 had stability problems. As a result, Pashinin made modifications to the second prototype, consisting of new outer wing panels with tapered leading and trailing edges to improve stability. Although an improvement, the I-21 still was not performing as expected, despite some promising speeds of over 480 km/h (300-mph) at sea level. The third prototype featured more extensive remodeling of the wings, with clipped wingtips (reducing wingspan by 1.57-m) and sweeping back the leading edges. In addition, the tailplane was also improved. This last prototype also was fitted with a ventral oil cooler

The third prototype displayed improved performance and handling, but officials complained of the I-21's need for an unacceptably long runway and its tricky character on landing. In the event, a planned pre-series run for five aircraft was canceled by Soviet officials, who likely felt the I-21 simply did not offer much more than types already in established production.

Specifications (I-21)

General characteristics

• Crew: One
• Length: 8.73 m (28 ft 7.7 in)
• Wingspan: 9.4m (30 ft 10.07 in)
• Height: (N/A)
• Wing area: 15.46 m² (50.86 ft²)
• Loaded weight: 2,670 kg (5,874 lbs)
• Powerplant: 1× Klimov M-105P V12 inline engine, (1,050 hp)

Performance

• Maximum speed: 580 km/h (360 mph)
• Range: 760 km (472 mi)
• Service ceiling: 10,600 m (34,776 ft)
• Rate of climb: 21 m/s (4,133 ft/min)
• Wing loading: 173 kg/m² (35.4 lb/ft²)

Armament

• 2 × 7.62 mm ShKAS machine guns, in wings, and one 20mm ShVAK cannon or 23mm BT-23 cannon firing through propeller hub.

References

References

• Green, William and Gordon Swanborough. The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. London: Salamander Books Ltd, 2002. ISBN 1-840-65269-1.

This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Pashinin I-21".