BRM Argos

{{short description|Portuguese ultralight aircraft}}

{{Use dmy dates|date=December 2022}}

{{Use British English|date=December 2022}}

{{Infobox Aircraft Begin

| name=Argos

| image=

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}}{{Infobox Aircraft Type

| type=Ultralight aircraft

| national origin=Portugal

| manufacturer=BRM Costruções Aeronáuticas

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| retired=

| status=In production (2015)

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}}

The BRM Argos is a Portuguese ultralight aircraft, designed and produced by BRM Costruções Aeronáuticas. The aircraft is supplied as a kit for amateur construction.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 33. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 36. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The Argos was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.

The aircraft is made from 6061-T6 aluminum sheet, with its cockpit strengthened with steel roll-over protection. Its {{convert|8.4|m|ft|1|abbr=on}} span wing has an area of {{convert|11.6|m2|sqft|abbr=on}} and electrically actuated flaps. Standard engines available are the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS, {{convert|85|hp|kW|0|abbr=on}} Jabiru 2200 and the {{convert|120|hp|kW|0|abbr=on}} Jabiru 3300 four-stroke powerplants. Cockpit access is by two gull-winged doors

Specifications (Argos)

{{Aircraft specs

|ref=Bayerl and BRM Costruções Aeronáuticas,{{cite web|url = http://www.landafrica.com/#as|title = Argos|accessdate = 13 May 2012|last = BRM Costruções Aeronáuticas|date = 1 March 2012}}

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=6.59

|length ft=

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|span m=8.4

|span ft=

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|height m=2.4

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|wing area sqm=11.6

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|gross weight kg=450

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|fuel capacity={{convert|70|L}}

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|eng1 number=1

|eng1 name=Rotax 912ULS

|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine

|eng1 kw=75

|eng1 hp=

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|max speed kmh=220

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|cruise speed kmh=190

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|stall speed kmh=60

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|ceiling m=4200

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|g limits=+4/-2

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}}

References

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