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Hanriot HD.1role : fighterfirst flight : operational : August 1917country : Francedesign : Pierre Dupontproduction : 831 aircraft (license built by Macchi in Italy)general information :Excellent fighter plane. The French armee de lair already had the famous Nieuport and SPAD fighters in its inventory and did not choose for this fine fighter plane. It was adopted by the Belgian and Italian air force who used the plane with great success. It was very agile in combat, strong and fast. In Italy it had to fight the Brandenburg D.1 fighter as well as Albatros fighters. Famous aces flew the HD.1 like Scaroni (26 victories) and Baracchini (21 victories) for Italy and Willy Coppens de Houthulst (37 victories) for Belgium.users : Belgium, Italycrew : 1armament : 1 synchronized 7.70 [mm] (0.303 in) Vickers machine-gun engine : 1 Le Rhone 9j air-cooled 9 -cylinder two-valve rotary engine 110 [hp](80.9 KW)dimensions : wingspan : 8.68 [m], length : 5.85 [m], height : 2.94[m] wing area : 18.2 [m^2]weights : max.take-off weight : 652 [kg] empty weight operational : 407 [kg] bombload : 0 [kg]performance : maximum speed : 184 [km/hr] at sea-level climbing speed : 392 [m/min] service ceiling : 6400 [m] endurance : 2.5 [hours] estimated action radius : 207 [km]description : 1-bay biplane with fixed landing gear and tail strut two spar upper and lower wing engines, landing gear, fuel and bombs in or attached to the fuselageairscrew : fixed pitch 2 -bladed tractor airscrew with max. efficiency :0.64 [ ] estimated diameter airscrew 2.36 [m] angle of attack prop : 26.63 [ ] coarse pitch reduction : 1.00 [ ] airscrew revs : 1100 [r.p.m.] pitch at Max speed 2.79 [m] blade-tip speed at Vmax and max revs. : 145 [m/s] calculation : *1* (dimensions) mean wing chord : 1.05 [m] calculated wing chord (rounded tips): 1.17 [m] wing aspect ratio : 8.28 [] gap : 1.21 [m] gap/chord : 1.15 [ ] seize (span*length*height) : 149 [m^3]calculation : *2* (fuel consumption) oil consumption : 4.9 [kg/hr] fuel consumption(cruise speed) : 21.6 [kg/hr] (29.5 [litre/hr]) at 56 [%] power distance flown for 1 kg fuel : 7.66 [km/kg] estimated total fuel capacity : 84 [litre] (61 [kg])calculation : *3* (weight) weight engine(s) dry : 147.0 [kg] = 1.82 [kg/KW] weight 18 litre oil tank : 1.6 [kg] oil tank filled with 0.6 litre oil : 0.5 [kg] oil in engine 0 litre oil : 0.4 [kg] fuel in engine 1 litre fuel : 0.4 [kg] weight 13 litre gravity patrol tank(s) : 1.9 [kg] weight cowling 3.2 [kg] weight airscrew(s) (wood) incl. boss & bolts : 19.0 [kg] total weight propulsion system : 172 [kg](26.5 [%]) *************************************************************** fuselage skeleton (wood gauge : 5.23 [cm]): 41 [kg] bracing : 1.7 [kg] fuselage covering ( 6.5 [m2] doped linen fabric) : 2.1 [kg] weight controls + indicators: 5.2 [kg] weight seats : 3.0 [kg] weight other details, lighting set, etc. : 5.1 [kg] weight 71 [litre] main fuel tank empty : 5.7 [kg] weight engine mounts & firewalls : 4 [kg] total weight fuselage : 68 [kg](10.4 [%]) *************************************************************** weight wing covering (doped linen fabric) : 12 [kg] total weight ribs (51 ribs) : 39 [kg] load on front upper spar (clmax) per running metre : 639.0 [N] load on rear upper spar (vmax) per running metre : 222.6 [N] total weight 8 spars : 28 [kg] weight wings : 78 [kg] weight wing/square meter : 4.28 [kg] weight 4 interplane struts & cabane : 5.1 [kg] weight cables (42 [m]) : 1.8 [kg] (= 43 [gram] per metre) diameter cable : 2.7 [mm] weight fin & rudder (0.9 [m2]) : 3.9 [kg] weight stabilizer & elevator (2.0 [m2]): 8.9 [kg] total weight wing surfaces & bracing : 98 [kg] (15.0 [%]) ******************************************************************* weight machine-gun(s) : 15.9 [kg] weight ammunition magazine(s) :1.8 [kg] weight Alkan-Hamy synchronization gear : 1.0 [kg] weight armament : 19 [kg] ******************************************************************** wheel pressure : 326.0 [kg] weight 2 wheels (650 [mm] by 76 [mm]) : 14.7 [kg] weight tailskid : 1.6 [kg] weight undercarriage with axle 13.7 [kg] total weight landing gear : 30.0 [kg] (4.6 [%] ******************************************************************* ******************************************************************** calculated empty weight : 387 [kg](59.3 [%]) weight oil for 3.0 hours flying : 14.6 [kg] weight ammunition (400 rounds) : 11.0 [kg] weight signal pistol with cartridges : 3.6 [kg] weight automatic pistol with spare magazines : 1.2 [kg] ******************************************************************* calculated operational weight empty : 417 [kg] (63.9 [%]) published operational weight empty : 407 [kg] (62.4 [%]) _____________ | o | ------------- " weight crew : 81 [kg] weight fuel for 1.5 hours flying : 32 [kg] ******************************************************************** operational weight : 530 [kg](81.3 [%]) estimated bomb load : 25 [kg] operational weight bombing mission : 555 [kg] fuel reserve : 29 [kg] enough for 1.34 [hours] flying possible additional useful load : 68 [kg] operational weight fully loaded : 652 [kg] with fuel tank filled for 100 [%] published maximum take-off weight : 652 [kg] (100.0 [%]) || I||==| || calculation : * 4 * (engine power) power loading (operational without bombload) : 6.56 [kg/kW] total power : 80.9 [kW] at 1100 [r.p.m] calculation : *5* (loads) manoeuvre load : 3.7 [g] at 1000 [m] limit load : 4.5 [g] ultimate load : 6.8 [g] load factor : 2.2 [g] design flight time : 2.00 [hours] design cycles : 275 sorties, design hours : 550 [hours] operational wing loading : 286 [N/m^2] wing stress (3 g) during operation : 200 [N/kg] at 3g emergency manoeuvre calculation : *6* (angles of attack) angle of attack zero lift : -1.16 ["] max. angle of attack (stalling angle) : 12.12 ["] angle of attack at max. speed : 0.93 ["]calculation : *7* (lift & drag ratios lift coefficient at angle of attack 0 :0.10 [ ] lift coefficient at max. angle of attack : 1.15 [ ] lift coefficient at max. speed : 0.18 [ ] induced drag coefficient at max. speed : 0.0022 [ ] drag coefficient at max. speed : 0.0344 [ ] drag coefficient (zero lift) : 0.0322 [ ]calculation : *8* (speeds stalling speed at sea-level (OW): 73 [km/u] landing speed at sea-level (OW without bombload): 87 [km/hr] min. drag speed (max endurance) : 110 [km/hr] at 3200 [m](power :34 [%]) min. power speed (max range) : 119 [km/hr] at 3200 [m] (power:36 [%]) max. rate of climb speed : 109.1 [km/hr] at sea-level cruising speed : 166 [km/hr] op 3200 [m] (power:59 [%]) design speed prop : 178 [km/hr] maximum speed : 184 [km/hr] op 100 [m] (power:99 [%]) climbing speed at sea-level (without bombload) : 325 [m/min]calculation : *9* (regarding various performances) take-off distance at sea-level : 252 [m] lift/drag ratio : 10.66 [ ] max. practical ceiling : 5875 [m] with flying weight :493 [kg] practical ceiling (operational weight): 5525 [m] with flying weight :530 [kg] practical ceiling fully loaded (mtow- 1 hour fuel) : 4575 [m] with flying weight :630 [kg] published ceiling (6400 [m] climb to 1500m (without bombload) : 5.11 [min] climb to 3000m (without bombload) : 12.36 [min] max. dive speed : 418.3 [km/hr] at 3575 [m] height load factor at max. angle turn 2.39 ["g"] turn radius at 500m: 48 [m] time needed for 360* turn 9.4 [seconds] at 500mcalculation *10* (action radius & endurance) operational endurance : 2.84 [hours] with 1 crew and 93 [kg] useful (bomb)load and 100.0 [%] fuel published endurance : 2.50 [hours] with 1 crew and possible useful (bomb) load : 100 [kg] and 88.1 [%] fuel action radius : 513 [km] with 1 crew and 20[kg] photo camera/radio transmitter or bombload max range theoretically with additional fuel tanks for total 232 [litre] fuel : 1301 [km] useful load with action-radius 250km : 105 [kg] production : 17.31 [tonkm/hour] oil and fuel consumption per tonkm : 1.53 [kg] _ I_==/ Literature : Praktisch handboek vliegtuigen deel 1 page 153 Fighters 1914-19 page 66 Janes fighting aircraft WWI page 114 DISCLAIMER Above calculations are based on published data, they must be regarded as indication not as facts. Calculated performance and weight may not correspond with actual weights and performances and are assumptions for which no responsibility can be taken. Calculations are as accurate as possible, they can be fine-tuned when more data is available, you are welcome to give suggestions and additional information so we can improve our program. For copyright on drawings/photographs/ content please mail to below mail address (c) B van der Zalm 29 Oktober 2019 contact : info.aircraftinvestigation@gmail.com python 3.7.4 , The listbelow showcases production numbers for all aircraft in the MilitaryFactory.com database. To keep page download times short, we have a minimum requirement of 100 aircraft produced. Hanriot HD.1. Single-Seat, Single Engine Biplane Fighter Aircraft. 1,200. 1973. Ilyushin IL-22 (Coot-B) Airborne Command Post (ACP) Aircraft. 1,200. 1970., Hanriot Production List. Browse All Aircraft by Manufacturer Home. There're 12 aircraft made by Hanriot. Tail Number Year Maker Model C/N Engines Seats Location 19309: 1917 Hanriot HD-1: 515: 1: 1: Italy 653: 0000 Hanriot HD-1: Not found 653: 1: 1:.
Usually, planes were identified by their year of build, number of seats, engine, and horsepower. Thus Hanriot's first aeroplane was the '1907 monoplane', type IV was the '1911 the designation HD. was kept for aircraft already in production, but the prefix was changed to LH. for new designs. Hanriot aircraft adopted the single letter 'H , However, French and British aircraft production was still essentially needed for domestic use so that deliveries to Belgium were slow and in limited numbers. To be able to rely on yet another source for fighter aircraft procurement, the Belgian authorities turned to the French constructor Hanriot which produced the nimble but very maneuverable , production : 17.31 [tonkm/hour] oil and fuel consumption per tonkm : 1.53 [kg] _ I_°==/ ° Literature : Praktisch handboek vliegtuigen deel 1 page 153. Fighters 1914-19 page 66. Jane´s fighting aircraft WWI page 114. DISCLAIMER Above calculations are based on published data, they must be. regarded as indication not as facts., The Hanriot HD.1 was a French World War I single seat fighter. Rejected for service with French squadrons in favour of the SPAD S.7, the type was supplied to the Belgians and the Italians with whom it proved highly successful. 831 of a total production of about 1200 were in fact produced by Italian companies under licence.. Development and Production. The Hanriot company produced a series of , The nimble Hanriot H.D.1 was never accepted by France's Aviation Militaire, probably because it used the same engine as the Nieuport 16 and 17, which was already in production.It found great proponents, though, in Italy and Belgium and (after the war) Switzerland. It was unusual in having pronounced dihedral in the upper wing but none in the lower, a design which may have improved pilot sight , Production list - Aviation website for aircraft and airline information (flight, photo, travel, fleet listing, production list of Airbus Boeing Douglas Embraer Dash, ATR, Sukhoi, Saab), plane photos for planespotters, flightlog database, aviation news, aviation store..