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Aeros-2

type of aircraft

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionNov 9, 2025
Entity authorityQ4688415
Source-derived summary

The Aeros-2 is a Ukrainian ultralight trike, designed and produced by Aeros of Kyiv. The aircraft is supplied as a complete ready-to-fly aircraft or as kit for amateur construction.

In the United States the design is marketed as the Venture and Velocity.

Design and development

Developed from the earlier Aeros-1, the Aeros-2 features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, tricycle landing gear and a single engine in pusher configuration.

The aircraft is made from square tubing, with its wing covered in Dacron sailcloth. Its 10 m (32.8 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The occupants are housed in streamlined fibreglass cockpit fairing. Engines available include the twin cylinder, two-stroke, liquid-cooled 64 hp (48 kW) Rotax 582 and the four cylinder four-stroke 80 hp (60 kW) Rotax 912UL and 100 hp (75 kW) 912ULS. Engine mounts for BMW and Subaru engines are also available. Available wings to be mated to the carriage are the Aeros Profi, Aeros Stranger, Aeros Stream and Aeros Still. The wing-mounting pylon is foldable, allowing the wing to be installed by one person.

Editorial summary

The public source identifies “Aeros-2” as type of aircraft. This brief keeps that definition visible, then builds a research path around Aeros-2, type and aircraft.

Editorial reviewA concise reference frame for defining the subject, testing terminology and identifying the institution closest to the evidence. The current 192-word lead offers orientation but no explicit four-digit date, so chronology should not be assumed. The selected authority fields contribute no independent date. Its value is orientation rather than verdict, with Aeros-2, type and aircraft providing the first useful test.
Editorial analysis

Why this record matters

A short description can identify a subject without explaining its stakes. For “Aeros-2”, the useful work is to connect “type of aircraft” to the records capable of establishing context and consequence.

Evidence profile

Named sources, stable identifiers and responsible institutions provide the strongest route from overview to verifiable evidence. The source revision retrieved here is dated Nov 9, 2025. The linked authority identifier is Q4688415. 1 of 1 selected statements include explicit references; 0 carry qualifiers and 0 use preferred rank.

Critical limits

A concise general-reference account can conceal disagreements about scope, terminology or the weight assigned to individual sources. The lead is largely declarative, so disagreement and counter-evidence require a deliberate search beyond the opening account. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

How to read it

Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.

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The closest primary source, responsible institution and strongest cited specialist reference.

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  1. Establish the record: confirm the title “Aeros-2”, its source revision and the description used here.
  2. Expand the search: follow Aeros-2 primary sources, Aeros-2 archive and Aeros-2 research across catalogues and specialist indexes.
  3. Test the account: compare the strongest cited source with the responsible institution’s current record and note any disagreement.

Questions for further research

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Source & attribution

This entry incorporates text from Aeros-2” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.