Aeros Still
title: "Aeros Still" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["ultralight-trike-wings"] topic_path: "general/ultralight-trike-wings" source: "https://en.wikipedia.org/wiki/Aeros_Still" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | Still |
| aircraft_type | Ultralight trike wing |
| national_origin | Ukraine |
| manufacturer | Aeros |
| status | In production (2013) |
| :: |
| name = Still | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Ultralight trike wing | aim = | outcome = | related = | national_origin = Ukraine | manufacturer = Aeros | design_group = | designer = | builder = | issuer = | status = In production (2013) | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = The Aeros Still is a Ukrainian single-surface ultralight trike wing, designed and produced by Aeros of Kyiv. The wing is widely used on Aeros trikes as well as by other ultralight aircraft manufacturers.
Design and development
The Still wing is a cable-braced, king post-equipped hang glider-style wing designed as a docile beginner and flight training wing for two-place trikes. It comes in one size, the Still-17, named for its metric wing area of 17.4 m2.
The wing is made from bolted-together aluminium tubing, with its single surface wing covered in Dacron sailcloth. The wing's crosstube is exposed and is of a floating design. Its 10.3 m span wing has a nose angle of 122°, an aspect ratio of 6.1:1 and uses an "A" frame weight-shift control bar.
Applications
Specifications (Still-17)
|ref=Bayerl and Aeros |prime units?=met General characteristics
|genhide=
|crew= |capacity= |length m= |length ft= |length in= |length note= |span m=10.3 |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm=17.4 |wing area sqft= |wing area note= |aspect ratio=6.1:1 |airfoil= |empty weight kg=45 |empty weight lb= |empty weight note=wing weight |gross weight kg=450 |gross weight lb= |gross weight note=maximum aircraft gross weight allowed |more general= Performance
|perfhide=
|max speed kmh= |max speed mph= |max speed kts= |max speed note= |cruise speed kmh=80 |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=50 |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh=105 |never exceed speed mph= |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=+4/-2 |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=25.9 |wing loading lb/sqft= |wing loading note=maximum |more performance=
References
References
- Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 198. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- [[Aeros]]. (2005). "Still".
- [[Aeros]]. (2005). "Still Performance".
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