Team Mini-Max AeroMax

{{Short description|American homebuilt aircraft}}

{{Use mdy dates|date=January 2022}}

{{Use American English|date=January 2022}}

{{Infobox aircraft begin

| name=AeroMax

| image=

| caption=

}}{{Infobox aircraft type

| type=Amateur-built aircraft and Light-sport aircraft

| national origin=United States

| manufacturer=Team Mini-Max

| designer=

| first flight=

| introduced=2012

| retired=

| status=In production (2012)

| primary user=

| more users=

| produced= 2012-present

| number built=

| developed from= ISON Airbike

| variants with their own articles=

}}

The Team Mini-Max AeroMax is an American amateur-built aircraft and light-sport aircraft, produced by Team Mini-Max of Niles, Michigan. The aircraft is supplied as a kit for amateur construction.Bernard, Mary and Suzanne B. Bopp: Mini-Max: AeroMax, Kitplanes, Volume 29, Number 12, December 2012, page 26. Belvoir Publications. {{ISSN|0891-1851}}

Design and development

Developed from the ISON Airbike, the AeroMax features a strut-braced high-wing, a single-seat open cockpit that is {{convert|14|in|cm|0|abbr=on}} wide, fixed conventional landing gear and a single engine in tractor configuration. The narrow fuselage allows the pilot to sit in the cockpit with his or her legs on the outside of the aircraft, with feet on the external rudder pedals.{{cite web|url = http://www.teammini-max.com/aircraft/aeromax/|title = AeroMax|accessdate = 22 November 2012|last = Team Mini-Max|year = 2012}}

The aircraft is made from pre-fabricated metal components and CNC laser-cut plywood parts. Its {{convert|28.4|ft|m|1|abbr=on}} span wing has an area of {{convert|127.7|sqft|m2|abbr=on}}, is supported by "V" struts and features fiberglass drooped wingtips. The main landing gear is made from sprung steel and mounts drum brakes. The elevator trim system is electric. The aircraft's recommended engine the {{convert|50|hp|kW|0|abbr=on}} Hirth F-23 two-stroke powerplant. Tricycle landing gear, tundra tires and floats are under development. Construction time from the supplied kit is estimated as 200–300 hours.

A tandem two seat model is also under development by the company.

As of August 2012, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.{{cite web|url = http://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xls|title = SLSA Make/Model Directory|accessdate = 21 November 2012|last = Federal Aviation Administration|date = 12 October 2012}}

Specifications (AeroMax)

{{Aircraft specs

|ref=Kitplanes and manufacturer

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=17

|length in=10

|length note=

|span m=

|span ft=28

|span in=5

|span note=

|height m=

|height ft=5

|height in=11

|height note=

|wing area sqm=

|wing area sqft=127.7

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=429

|empty weight note=

|gross weight kg=

|gross weight lb=738

|gross weight note=

|fuel capacity={{convert|13|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Hirth F-23

|eng1 type=twin cylinder, air-cooled, two stroke aircraft engine

|eng1 kw=

|eng1 hp=50

|prop blade number=3

|prop name=composite

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=75

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=69

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=32

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=110

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=+3.5/-1.8

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1500

|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=5.8

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}