| General Information | |
|---|---|
| Type | Yak-7 M-105PA |
| Function | Fighter |
| Year | 1941 |
| Crew | 1 |
| Powerplant | |
| Type | M-105PA |
| Takeoff Power | 1100hp |
| Power at 0m | 1020hp |
| Power at 2000m | 1100hp |
| Size | |
| Length | 8.50m |
| Height | ?m |
| Wingspan | 10.0m |
| Wing area | 17.15m2 |
| Weights and loads | |
| Empty | 2477kg |
| Loaded | 2960kg |
| Wing Load (kg/m2) | 173 |
| Power load (kg/hp) | 2.69 |
| Speed | |
| at 0m | 471km/h |
| at 4500m | 560km/h |
| Landing | 136km/h |
| Maneuverability | |
| Turn time | 24sec |
| Roll | |
| Takeoff | 375m |
| Landing | 550m |
| Range | |
| Practical | 643km |
| Ceiling | |
| Ceiling | 9250m |
| Climb | |
| 5000m | 6.8min |
| Payload | |
| Fuel | 305kg |
| Cargo | ~100kg in rear cabin |
| Seats | (1) |
| Armament | |
| Gun Type | 1*20mm ShVAK |
| Position | through the hub |
| Ammo | 120 |
| Gun Type | 2*7.62mm ShKAS |
| Position | engine cowling |
| Ammo | 2*750 |
| Salvo | 1.73 (kg/sec) |
| Rockets | 6*RS-82 |
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Yak-7 with M-105PA engine and VISh-61P propeller was a conversion of the Yak-7UTI trainer into single-seat combat aircraft. Conversion was performed at Factory N°301 following initiative of the leading engineer K.V.Sinelschikov and team of the Yakovlev OKB members. This team was assigned to the factory to assist in mass production of the Yak-7UTI. They used series aircraft N°04-11 and introduced following changes:
Tailwheel and the canopy remained same as on Yak-7UTI, and except the RS-82 rails both aircraft had identical appearance. New fighter was more advanced than contemporary series Yak-1. It had following advantages:
Empty space of the second cockpit could be used in a number of ways, quite unusual for fighters:
Technical commission of the OKB rated Yak-7 fighter as a perspective design allowing numerous modifications. First reaction of A.S.Yakovlev was skeptical, but after detailed study he approved the conversion. He presented the the Yak-7 design to the top officials, and, in turn, gained support. In August 1941 production was ordered on two factories - N°153 (Novosibirsk) and N°301 (Moscow).
Production of the original Yak-7 was not really a big series one: 51 were assembled in Moscow (Factory N°301) in September-October, and eleven more at Factory N°153 in December 1941. Pause in November was caused by Factory N°301 evacuation and integration into plant N°153.
Yak-7 fighter N°04-11 was evaluated at NII VVS and received positive resume. Detailed studies of aircraft handling were carried out by factory N°153 test pilot A.N.Lazarev and TsAGI team. Yak-7 was considered superior against LaGG-3 and spin safe. Spin could be stopped immediately by placing stick and pedals into neutral position.
In September 1941 Yak-7 N°06-05 with RS-82 launchers installed was sent to the NIPAV (Scientific Trial Range of the Aircraft Armament). Better stability of the Yak-7 and decreased salvo proved its advantage over rocket-armed LaGG-3 and MiG-3:
| Aircraft | Yak-7 | LaGG-3 | MiG-3 |
|---|---|---|---|
| Firing Altitude (m) | 600 | 800 | 500 |
| Aircraft speed (km/h) | 400 | 400 | 400 |
| Dive Angle (deg) | 50...60 | 45...50 | 45...60 |
| Salvo | 2...4 | 4 | 4...6 |
| Range scatter (m) | 8...20 | 5...34 | 20...82 |
| Transverse scatter (m) | 6...18 | 9...29 | 15...39 |
Tests also revealed defects in landing gear, pneumatic system and insufficient assembly quality. Original Yak-7 fighter was replaced in production by improved Yak-7A.
| References | |
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| Created December 17, 2000 |
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