1. Design and development
    LH.41.02  LH.42 

2. Operational history

3. Variants

4. Specifications (LH.41)

5. References

The Lorraine Hanriot LH.41 was a single-seat racing aircraft designed and built in France specifically to compete in the Coupe Michelin air races, held in France.

Design and development

The LH.41 was a small low-wing, cantilever monoplane built largely of wood with fabric and plywood skinning. The LH.41 was supported on a wide-track strut mounted undercarriage, incorporating oleo-pneumatic shock-absorbers, with a tail-skid.^[1][2]

For initial flight testing the LH.41 was fitted with a {{convert|240|hp|abbr=on|disp=flip}} Lorraine 7Mb Mizar 7-cylinder radial engine with a distinctive oil cooler on the port side of the fuselage forward of the cockpit. After initial testing the LH.41, re-engined with the intended {{convert|230|hp|abbr=on|disp=flip}} Lorraine 9Nb driving a Levasseur metal fixed pitch propeller fitted with a dorsal oil cooler in place of the side mounted cooler. The 9Nb was fitted with a short chord Townend ring by the time the race began.^[1][2]

LH.41.02

Lorraine-Hanriot recovered the engine from the wreckage of the LH.41, tested it to ensure it was serviceable and fitted it to a new airframe, dubbed LH.41.02 (aka LH.41/2, or LH.41-2). The airframe was refined to give less drag, removing exterior bracing cables on the tail-unit and fully enclosing the engine in a NACA cowling.^[3]

LH.42

Another airframe was built, essentially identical to the LH.41.02, but with further improvements, including faired-in undercarriage legs.^[3]

Operational history

The LH.41 first flew in May 1930 and was duly entered in the 1929/1930 Coupe Michelin, flown by Marcel Haegelen. The LH.41 was beating the competition until an accident upon landing at Reims destroyed the aircraft and seriously injured Haegelen, after landing in tall grass.^[2]

After the unfortunate demise of the LH.41.01 at Reims, Lorraine-Hanriot enterred the LH.41.02 in the 1930/1931 Coupe Michelin air race, which Haegelen won at an average speed of {{convert|255.6|km/h|kn mph|abbr=on}}, flying {{convert|2632|km|nmi mi|abbr=on}} in 11 hours 37 minutes 21 seconds, including refuelling, take-offs and landings.^[3]

The LH.42 was flown by Haegelen in the 1931/1932 Coupe Michelin air race on 12 August 1932, achieving victory again, at an average speed of {{convert|254.36 |km/h|kn mph|abbr=on}}, flying {{convert|2632|km|nmi mi|abbr=on}} in 10 hours 20 minutes 21 seconds, including refuelling take-offs and landings.^[3]

After the 1931/1932 Coupe Michelin victory, Haegelen proposed a world record speed attempt for a {{convert|500|km|abbr=on}} closed -circuit. Taking off on 31 August 1932 Haegelen completed the course but was unable to land at Étampes, on his return, due to bad weather. Diverting to Tours was fruitless, as the area was shrouded in fog. After circuiting Tour hoping for the fog to lift, Haegelen was forced to bail-out when the fuel was exhausted. The LH.42 continued on alone until it crashed near the Château du Loire.^[3]

Variants

LH.41.01

A racing aircraft, primarily intended to compete in the Coupe Michelin. The sole example was destroyed in an accident during the 1929/1930 Coupe Michelin race.

LH.41.02

A second machine built fitted with the Lorraine 9Nb recovered from the wreckage of the LH.41.01 driving a Ratier metal airscrew. Flown by Haegelen to victory in the 1930/1931 Coupe Michelin air race.^[3]

LH.42

The LH.41.02 developed with an all-metal fuselage, increased fuel capacity, more refined aerodynamic features and fully cowled Lorraine 9Nb engine up-rated to {{convert|240|hp|abbr=on|disp=flip}} driving a Levasseur-Ratier metal airscrew. The LH.42 crashed during a world record attempt due to bad weather.^[3]

Specifications (LH.41)

|genhide=
|crew=1
|length m=6.87
|length ft=
|length in=
|length note=
|span m=10.2
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=14
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=950
|empty weight lb=
|empty weight note=
|gross weight kg=1150
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|350|l|USgal impgal|abbr=on}}
|more general=

|eng1 number=1
|eng1 name= Lorraine 9Nb
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 kw=
|eng1 hp=230
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=2
|prop name=Levasseur metal fixed pitch propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=

|perfhide=
|max speed kmh=260
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=85
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=0.143 kW/kg (0.0872 hp/lb)
|more performance=
|avionics=
}}

References

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• White Space (film)
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