The Ion Aircraft Ion is a two-seat, twin boom, pusher configuration light aircraft based on the DreamWings Valkyrie. It was still in development in 2010 but is intended either for homebuilding from kits or flyaway production, with versions meeting US and European rules.
By November 2020 production had not started and the company was for sale.[2]Geode Capital Management completed the acquisition of Ion Aircraft on 10 September 2021. The company is now called Gaea Capital Management.[3]
The Ion Aircraft Ion is a development of the DreamWings Valkyrie, a twin boom, pusher configuration ultralight aircraft which flew for the first time in 1999. The Valkyrie generated considerable interest and many potential customers, but DreamWings became bankrupt in 2001. The project was later restarted by a customer group under the name of Ion Aircraft[4] and the part-built prototype of the Ion was displayed at Oshkosh in July 2005, though the first "hops" were not made until July 2007.[5] Whilst the Valkyrie and the Ion share the share twin boom, single pusher engine, mid-wing layout, have tricycle undercarriages and seat two in tandem, they differ significantly. In particular the Valkyrie's strongly swept and tapered fins, combined with a trailing low set horizontal tail, which extended beyond the booms, have been replaced with swept, parallel chord fins with a constant chord tailplane linking their upper tips. Unlike the Valkyrie, the Ion does not have a canard.[5]
Much of the Ion is made of composite materials; the fuselage pod, the wing centre section within the booms, the booms themselves and the empennage are all formed from carbon fiber/epoxypre-pregs. Outboard of the booms the wings are of bonded aluminium. The wings carry plain piano hingedailerons. The engine cover is GRP. The cockpit has a single piece canopy, shaped to allow the rear seat to be 8.5 in (220 mm) above the forward one, giving its occupant better vision. The prototype has fixed, aluminium cantilever spring main undercarriage legs and has been flown with and without wheel fairings. The mainwheels have hydraulic brakes and the nosewheel castors.[5][6]
Several options are to be offered, including a 3 ft 6 in (1050 mm) shorter[7] span wing which will raise the cruising speed by 25 mph (41 km/h; 22 kn) but also increase the stall speed by 32%, a retractable undercarriage and a ballistic recovery parachute. Kits will be offered to meet either US Light-Sport Aircraft (LSA) rules or European microlight regulations but flyaway aircraft will be built to LSA rules. Other engines, such as Rotax variants in the 100-115 hp (75-86 kW) power range may be fitted.[5]
In the two years after its first flight in 2007, the Ion prototype flew about 60 hours, some with a Jabiru 3300 six cylinder engine which experienced cooling problems but from May 2009 with a 100 hp (75 kW) Rotax 912ULSflat four engine.[5] In 2010 it appeared at AirVenture, Oshkosh under its own power with a ventral air intake and a new three blade propeller.[8] The second prototype was under construction but not registered in mid-2011.[8] The Ion will not be offered for sale until flight tests are completed.[5]
By November 2020 the company was up for sale with the principals indicating that, while they had developed the aircraft they lacked expertise in starting production. They indicated that they wished to sell the company rather than let the project die.[2] Geode Capital Management purchased Ion Aircraft on 10 September 2021. The company is now called Gaea Capital Management.[3]
Cruise speed: 152 mph (244 km/h, 132 kn) at 75% power
Stall speed: 43 mph (69 km/h, 37 kn) flaps down
g limits: +4.4/-2.2
Rate of climb: 1,610 ft/min (8.2 m/s) maximum at sea level
Take-off run: 500 ft (153 m)
References
^Vandermeullen, Richard: 2012 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 56. Belvoir Publications. ISSN 0891-1851
^ abIon Aircraft (12 November 2020). "Ion Aircraft is for sale!". www.ionaircraft.com. Archived from the original on 27 May 2021. Retrieved 27 May 2021.
^ ab"Geode Capital Management - Opportunities, development, win-win situation". ugcm.us. Archived from the original on 12 September 2021. Retrieved 12 September 2021.
^ abcJackson, Paul (2011). Jane's All the World's Aircraft 2012-13. Coulsdon, Surrey: IHS Global. p. 842. ISBN978-0-7106-3000-1.
^ abcBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 126. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
External links
Wikimedia Commons has media related to Ion Aircraft Ion.
Official website
January 17, 2023
aircraft, seat, twin, boom, pusher, configuration, light, aircraft, based, dreamwings, valkyrie, still, development, 2010, intended, either, homebuilding, from, kits, flyaway, production, with, versions, meeting, european, rules, ionion, airventure, 2010role, . The Ion Aircraft Ion is a two seat twin boom pusher configuration light aircraft based on the DreamWings Valkyrie It was still in development in 2010 but is intended either for homebuilding from kits or flyaway production with versions meeting US and European rules IonIon at AirVenture 2010Role Two seat light aircraftNational origin United StatesManufacturer Ion AircraftFirst flight 17 July 2007Number built One 2011 1 Developed from DreamWings ValkyrieIon prototype at AirVenture 2010 ION 100 ION 100 By November 2020 production had not started and the company was for sale 2 Geode Capital Management completed the acquisition of Ion Aircraft on 10 September 2021 The company is now called Gaea Capital Management 3 Contents 1 Design and development 2 Proposed variants 3 Specifications LSA Rotax 912ULS estimated performance 4 References 5 External linksDesign and development EditThe Ion Aircraft Ion is a development of the DreamWings Valkyrie a twin boom pusher configuration ultralight aircraft which flew for the first time in 1999 The Valkyrie generated considerable interest and many potential customers but DreamWings became bankrupt in 2001 The project was later restarted by a customer group under the name of Ion Aircraft 4 and the part built prototype of the Ion was displayed at Oshkosh in July 2005 though the first hops were not made until July 2007 5 Whilst the Valkyrie and the Ion share the share twin boom single pusher engine mid wing layout have tricycle undercarriages and seat two in tandem they differ significantly In particular the Valkyrie s strongly swept and tapered fins combined with a trailing low set horizontal tail which extended beyond the booms have been replaced with swept parallel chord fins with a constant chord tailplane linking their upper tips Unlike the Valkyrie the Ion does not have a canard 5 Much of the Ion is made of composite materials the fuselage pod the wing centre section within the booms the booms themselves and the empennage are all formed from carbon fiber epoxy pre pregs Outboard of the booms the wings are of bonded aluminium The wings carry plain piano hinged ailerons The engine cover is GRP The cockpit has a single piece canopy shaped to allow the rear seat to be 8 5 in 220 mm above the forward one giving its occupant better vision The prototype has fixed aluminium cantilever spring main undercarriage legs and has been flown with and without wheel fairings The mainwheels have hydraulic brakes and the nosewheel castors 5 6 Several options are to be offered including a 3 ft 6 in 1050 mm shorter 7 span wing which will raise the cruising speed by 25 mph 41 km h 22 kn but also increase the stall speed by 32 a retractable undercarriage and a ballistic recovery parachute Kits will be offered to meet either US Light Sport Aircraft LSA rules or European microlight regulations but flyaway aircraft will be built to LSA rules Other engines such as Rotax variants in the 100 115 hp 75 86 kW power range may be fitted 5 In the two years after its first flight in 2007 the Ion prototype flew about 60 hours some with a Jabiru 3300 six cylinder engine which experienced cooling problems but from May 2009 with a 100 hp 75 kW Rotax 912ULS flat four engine 5 In 2010 it appeared at AirVenture Oshkosh under its own power with a ventral air intake and a new three blade propeller 8 The second prototype was under construction but not registered in mid 2011 8 The Ion will not be offered for sale until flight tests are completed 5 By November 2020 the company was up for sale with the principals indicating that while they had developed the aircraft they lacked expertise in starting production They indicated that they wished to sell the company rather than let the project die 2 Geode Capital Management purchased Ion Aircraft on 10 September 2021 The company is now called Gaea Capital Management 3 Proposed variants EditIon 100 Kit LSA rules fixed undercarriage 6 9 Ion 105 Kit US Experimental amateur built rules retractable undercarriage short span wings Ion 110 Kit for European rules 6 9 Ion 105 Kit European microlight rules Ion 120 Flyaway LSA rules 6 9 Specifications LSA Rotax 912ULS estimated performance EditData from Jane s All the World s Aircraft 2012 13 8 General characteristicsCrew Pilot Capacity 1 passenger Length 24 ft 0 in 7 32 m Wingspan 32 ft 6 in 9 91 m Height 6 ft 5 in 1 96 m Fuel capacity 120 lb 54 kg Useful load 552 lb 250 kg Powerplant 1 Rotax 912ULS Air and water cooled flat four 100 hp 75 kW Propellers 3 bladed Warp Drive carbon fibre pusherPerformance Cruise speed 152 mph 244 km h 132 kn at 75 power Stall speed 43 mph 69 km h 37 kn flaps down g limits 4 4 2 2 Rate of climb 1 610 ft min 8 2 m s maximum at sea level Take off run 500 ft 153 m References Edit Vandermeullen Richard 2012 Kit Aircraft Buyer s Guide Kitplanes Volume 28 Number 12 December 2011 page 56 Belvoir Publications ISSN 0891 1851 a b Ion Aircraft 12 November 2020 Ion Aircraft is for sale www ionaircraft com Archived from the original on 27 May 2021 Retrieved 27 May 2021 a b Geode Capital Management Opportunities development win win situation ugcm us Archived from the original on 12 September 2021 Retrieved 12 September 2021 Ion history Retrieved 6 February 2012 a b c d e f Jackson Paul 2011 Jane s All the World s Aircraft 2011 12 Coulsdon Surrey IHS Jane s pp 770 771 ISBN 978 0 7106 2955 5 a b c d Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 111 Flying Pages Europe SARL 2015 ISSN 1368 485X Ion details Retrieved 6 February 2012 a b c Jackson Paul 2011 Jane s All the World s Aircraft 2012 13 Coulsdon Surrey IHS Global p 842 ISBN 978 0 7106 3000 1 a b c Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 126 WDLA UK Lancaster UK 2011 ISSN 1368 485XExternal links Edit Wikimedia Commons has media related to Ion Aircraft Ion Official website Retrieved from https en wikipedia org w index php title Ion Aircraft Ion amp oldid 1123933391, wikipedia, wiki, book, books, library,
