il2_specs

Hanriot HD.1

描述

The Hanriot HD.1 was developed by Pierre Dupont in the summer of 1916 for the Hanriot company as a classical biplane made mostly of wood with two-spar wings (the rudder frame and the nose part were metal). The upper wing had a small V-angle while the lower one was straight. There were 3 fuel tanks in the fuselage: two behind the engine and one more behind the pilots back.

At first, the HD.1 was meant to take over from the older Nieuport 11 and 17 planes, but the new Spad 7s were already in use on the front lines and got positive feedback from pilots for their in-line engines. Meanwhile, Nieuport squadrons still used Le Rhone engines. As a result, the French Air Force (Aviation Militaire) decided not to switch to HDs as it wasnt cost-effective, and the acquisition was canceled.

However, the Entente allies found this plane attractive - it was more firm, maneuverable, and slightly better than the Nieuport in general. The Italian Air Force (Aviazione Militaire) was the first to order this plane. Societa Nieuport-Macchi started manufacturing HDs in November 1916, and in the summer of 1917, the first Hanriots were delivered to the front lines. By the end of the war, the Italians had 831 Hanriots. The Belgian Air Force, Aeronautique Militaire Belge, ranked second in buying these new planes, and the French Hanriot manufacturer constructed 125 aircraft. Belgian squadrons began flying HD1s on August 22, 1917, and they used them effectively, especially the Belgian aces like Coppens, de Meulemeester, and Olieslagers.

Engine: 9 cyl. rotary Le Rhone 9Jby 130 hp

Dimensions
Height: 2940 mm
Length: 5850 mm
Wing span: 8700 mm
Wing surface: 18.2 sq.m

Weight
Empty weight: 406.9 kg
Takeoff weight: 612.1 kg
Fuel capacity: 104 l
Oil capacity: 18 l

Climb rate
1000 m: 2 min. 39 sec.
2000 m: 5 min. 45 sec.
3000 m: 9 min. 22 sec.
4000 m: 14 min. 19 sec.
5000 m: 20 min. 52 sec.
6000 m: 31 min. 39 sec.

Maximum airspeed (IAS)
sea level — 188 km/h
1000 m — 179 km/h
2000 m — 169 km/h
3000 m — 159 km/h
4000 m — 149 km/h
5000 m — 138 km/h
6000 m — 126 km/h

Service ceiling 6620 m

Endurance — 2 h.

Armament
Forward firing: 1 x Vickers Mk.I 7.69 mm, 500 rounds per barrel.

References
1) Windsock Datafile 12 - Hanriot HD.1, by J.M. Bruce.

修改

“气球”机枪

Vickers “Balloon” gun
Ammo：250发11.43mm弹药
弹丸重量：17.5 g
膛口速度：610 m/s
枪炮重量：13 kg
弹药重量：20 kg
射速：600 rpm
总重：33 kg

驾驶舱照明

用于夜间飞行的驾驶舱照明灯
增加质量：1 kg

罗盘

L.麦克森型罗盘
增加质量：1 kg

勒克雷蒂安（LeChretien）瞄准具

勒克雷蒂安（LeChretien）折射型直筒瞄准具
增加质量：1 kg


Lewis Overwing

Overwing mounted additional Lewis machinegun with changeable position.
弹药：388发7.69mm弹药（4个弹鼓，每个97发）
弹丸重量：11 g
膛口速度：745 m/s
射速：550 rpm
枪炮重量：8 kg（无弹鼓）
基座重量：3 kg
弹药重量：16 kg
总重：27 kg
预期速度损失：5 km/h