Evektor EPOS

{{Short description|Czech electric ultralight}}

{{Use dmy dates|date=February 2023}}

{{Use British English|date=February 2023}}

{{Notability|date=January 2023}}

{{Infobox aircraft begin

| name= EPOS

| image=

| caption=

}}{{Infobox aircraft type

| type=Electric aircraft

| national origin=Czech Republic

| manufacturer=Evektor-Aerotechnik

| designer=

| first flight=March 2013

| introduced=2013

| retired=

| status=Under development (2015)

| primary user=

| more users=

| produced=

| number built=

| developed from=

| variants with their own articles=

}}

The Evektor EPOS ("Electric powered small aircraft"),{{cite web | title=First flight of the SportStar EPOS | publisher=Evektor | date=28 March 2013| url=https://www.evektor.com/post/first-flight-of-the-sportstar-epos}} also called the SportStar EPOS, is a Czech electric ultralight and light-sport aircraft under development by Evektor-Aerotechnik of Kunovice. It was introduced at the AERO Friedrichshafen show in 2013.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 48. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

The aircraft first flew at the end of March 2013.

Design and development

The EPOS is based upon the Evektor SportStar RTC, a Fédération Aéronautique Internationale microlight and CS-LSA light-sport aircraft. It uses the RTC model's fuselage, mated to a new wing of longer span. It features a cantilever low-wing, an enclosed cockpit with two-seats-in-side-by-side configuration under a bubble canopy, fixed tricycle landing gear and a single electric motor in tractor configuration.

The aircraft is predominantly made from aluminum sheet. The initial electric motor employed was the Rotex RE X907 of {{convert|67|hp|kW|0|abbr=on}} at 330 volts. In 2014 the design was upgraded with a Rotex RE BB 90-5, a brushless, DC, liquid-cooled powerplant that produces {{convert|100|hp|kW|0|abbr=on}} at 3,000 rpm and weighs {{convert|20|kg|lb|0|abbr=on}}. It is controlled by a MGM Compro HBC-Series V7, 300400/EPOS1 controller with a maximum continuous current of 300 amperes and a maximum supply voltage of 400 volts. Power is supplied by 4 battery containers each with 45 Kokam Company, Ltd. SLPB100216216H cells of 40Ah capacity{{Cite web|url=https://liionbms.com/pdf/kokam/SLPB100216216H.pdf|title=Cell Specification Data - SLPB 100216216H|publisher=Kokam Company, Ltd.}} connected in series, producing 378 volts.{{cite web|url = https://www.evektoraircraft.com/en/sportstar-epos|title = SportStar EPOS+|accessdate = 18 February 2017|author=Evektor-Aerotechnik|year = 2017}}

Specifications (EPOS+)

{{Aircraft specs

|ref=Tacke and manufacturer

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=5.980

|length ft=

|length in=

|length note=

|span m=10.462

|span ft=

|span in=

|span note=

|height m=2.476

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=285

|empty weight lb=

|empty weight note=without batteries, 316 kg (697 lbs) with four battery containers.

|gross weight kg=600

|gross weight lb=

|gross weight note=

|fuel capacity=7,200Ah (4 containers each with 45 cells of 40 Ah capacity)

|more general=

|eng1 number=1

|eng1 name=Rotex RE BB 90-5

|eng1 type=brushless, DC, liquid cooled electric motor

|eng1 kw=75

|eng1 hp=

|prop blade number=3

|prop name=VZLÚ model V332-3A1 composite

|prop dia m=1.625

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=140

|max speed note=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=92

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=39

|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=

|endurance=1 hour with four battery containers, each with 45 cells

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|power/mass=

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}}

References

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