Brochet MB.60

{{Short description|1940s French light aircraft}}

{{Infobox aircraft begin

| name=MB.60 Barbastelle

| image=

| caption=

}}{{Infobox aircraft type

| type=Work plane

| national origin=France

| manufacturer=Brochet

| designer=Maurice Brochet

| first flight=24 June 1949

| introduced=

| retired=

| status=

| primary user=

| number built=1

| developed from=

| variants with their own articles=

}}

The Brochet MB.60 Barbastelle was a French two-seater work plane built by Maurice Brochet in the late 1940s.

Design and development

The MB.60 was a high-wing monoplane with a closed cabin. Although a two seater like the Brochet MB.50, it was distinguished by an airfoil without sweep-back, a raised upper deck of the rear fuselage and a fixed landing gear with split axle. Power came from a 83 horsepower Salmson 5-cylinder radial engine.

The only MB.60 to be completed (registered F-BFKT) took to the air on 24 June 1949 in Chavenay, piloted by André Deschamps. In the following July it was subjected to glider towing tests and presented in August at the 2nd National RSA rally before passing the certification tests. With Brochet working on the Brochet MB.70, the sole MB.60 was sold to a flying club and used as a glider tug. By the end of 1951 it had totaled 2,000 cycles.{{cite web|url=http://avions.brochet.free.fr/Histoire4.html |title=Avions Maurice Brochet Neauphle Le Chateau |publisher=Avions.brochet.free.fr |date= |accessdate=2020-04-06}}

Specifications

{{Aircraft specs

|ref=Avions Maurice Brochet Neauphle Le Chateau

|prime units?=met

|crew=1

|capacity=1 passenger

|length m=5.80

|length ft=

|length in=

|span m=8.0

|span ft=

|span in=

|height m=

|height ft=

|height in=

|wing area sqm=9.40

|wing area sqft=

|empty weight kg=

|empty weight lb=

|gross weight kg=

|gross weight lb=

|fuel capacity=

|eng1 number=1

|eng1 name=Salmson

|eng1 type=air-cooled radial engine

|eng1 hp=83

|eng1 note=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|perfhide=y

|max speed kmh=

|max speed mph=

|max speed kts=

|max speed mach=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|range km=

|range miles=

|range nmi=

|ceiling m=

|ceiling ft=

|climb rate ms=

|climb rate ftmin=

|more performance=

|avionics=

}}

References

{{reflist}}

Further reading

  • {{cite book |last=Gaillard |first=Pierre |title=Les Avions Francais de 1944 a 1964 |year=1990 |publisher=Editions EPA |language=French |location=Paris |isbn=2-85120-350-9 |page=87}}