Impuls IC

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title: "Impuls IC" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["hang-gliders"] description: "German hang glider" topic_path: "general/hang-gliders" source: "https://en.wikipedia.org/wiki/Impuls_IC" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary German hang glider ::

::data[format=table title="Infobox aircraft"]

Field	Value
name	IC
aircraft_type	Hang glider
national_origin	Germany
manufacturer	Impuls
status	Production completed
::

| name = IC | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Hang glider | aim = | outcome = | related = | national_origin = Germany | manufacturer = Impuls | design_group = | designer = | builder = | issuer = | status = Production completed | 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 Impuls IC is a German high-wing, single-place, hang glider that was designed and produced by Impuls of Munich.

The aircraft is no longer in production.

Design and development

The Impuls IC was designed as the company's attempt to create an intermediate hang glider which would be a natural progressive step for students from its beginner wings. The IC is certified as DHV Class 2.

The aircraft is made from aluminum tubing, with the wing covered in Dacron sailcloth. Its 10.1 m span wing is cable braced from a single kingpost. The nose angle is 126° and the aspect ratio is 6.7:1. Pilot hook-in weight range is 60 to.

The IC sold for €3950 in 2003.

Specifications (IC)

|ref=Bertrand |prime units?=met General characteristics

|genhide=

|crew=one |capacity= |length m= |length ft= |length in= |length note= |span m=10.1 |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm=15.2 |wing area sqft= |wing area note= |aspect ratio=6.7:1 |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |more general= Performance

|perfhide=Y

|max speed kmh= |max speed mph= |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |g limits= |roll rate= |glide ratio= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |more performance=

|see also= |related= |similar aircraft= |lists=

References

References

1. Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 46. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X
2. Impuls. (n.d.). "Die Impuls Flugdrachen GmbH hat die Produktion von Fluggeräten eingestellt. (German language)".

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