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URMV-3 IS-2

URMV-3 IS-2 is a science topic covered in the lgStudy science library. This page brings together a partial reference excerpt, illustrations, worked examples, real-world applications and a short study plan, so you can understand URMV-3 IS-2 rather than just read about it. In short: The IS-2 was an intermediate training glider designed by Iosif Şilimon and built in Romania in the 1950s at the URMV-3 (Rom: Uzinele de Reparatii Material Volant-3 - Glider repair and manufacture factory) factory at Brașov. Design and development The IS-2 was designed as an intermediate training glider.

Key takeaways

  • URMV-3 IS-2 belongs to science; place it in that map before memorising details.
  • Learn the definition first, then one example that makes the definition concrete.
  • Connect URMV-3 IS-2 to a quantity you can measure, compute or draw — that is where exam questions come from.
  • Reproduce the core statement of URMV-3 IS-2 from memory before moving on to harder problems.

Reference excerpt

The IS-2 was an intermediate training glider designed by Iosif Şilimon and built in Romania in the 1950s at the URMV-3 (Rom: Uzinele de Reparatii Material Volant-3 - Glider repair and manufacture factory) factory at Brașov.

Design and development The IS-2 was designed as an intermediate training glider. Construction was largely of wood with fabric and plywood skinning, similar to the Grunau Baby pre-war German glider. Very little is known of the IS-2's development or operational history. Of conventional configuration with high-set cantilever wings and cruciform tail-unit, the IS-2 was also flown with an increased span wing.

Specifications (IS-2) Data from The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume IIGeneral characteristics Crew: 1 Length: 6.54 m (21 ft 5 in) Wingspan: 12.3 m (40 ft 4 in) Height: 1.05 m (3 ft 5 in) at cockpit Wing area: 14.7 m2 (158 sq ft) Aspect ratio: 10.3 Airfoil: Root:Göttingen 535, Mid Göttingen 535, Tip Göttingen 676 Empty weight: 152 kg (335 lb) Gross weight: 250 kg (551 lb) Performance

Stall speed: 42 km/h (26 mph, 23 kn) Never exceed speed: 180 km/h (110 mph, 97 kn) *Rough air speed max: 130 km/h (81 mph; 70 kn) Aerotow speed: 110 km/h (68 mph; 59 kn) Winch launch speed: 80 km/h (50 mph; 43 kn) Terminal velocity: with full air-brakes at max all-up weight 180 km/h (112 mph; 97 kn) g limits: +4 -2.2 at 185 km/h (99.9 kn) Maximum glide ratio: 20 at 69 km/h (43 mph; 37 kn) Rate of sink: 0.77 m/s (152 ft/min) at 32.9 mph; 28.6 kn (53 km/h) Wing loading: 17 kg/m2 (3.5 lb/sq ft)

See also

Aircraft of comparable role, configuration, and era

Grunau Baby Slingsby Cadet Slingsby Kirby Tutor

Related lists List of gliders

Notes

References

Worked examples

Example 1 — a first encounter with URMV-3 IS-2

Start with the simplest possible case. Write down what URMV-3 IS-2 claims or describes in one sentence, then invent the smallest concrete situation in which that sentence is true. In science, the smallest case is usually a single object, a single equation or a single measurement. Check that every symbol or term in your sentence has a meaning in that case.

Example 2 — changing one variable

Take the situation from Example 1 and change exactly one quantity: double it, halve it, or set it to zero. Predict what should happen to URMV-3 IS-2 before you calculate. Comparing your prediction with the result is the fastest way to find out whether you understand the idea or only the words.

Example 3 — an exam-style question

Typical questions about URMV-3 IS-2 ask you to (a) state it precisely, (b) apply it to given data, and (c) explain a limitation. Practise writing all three answers in under five minutes; the third part is what separates a full-mark answer from an average one.

Applications of URMV-3 IS-2

In research
URMV-3 IS-2 appears in science research whenever the underlying quantities have to be modelled precisely. Papers usually cite it as a starting assumption and then explore where it breaks down.
In technology and industry
Engineering practice reuses URMV-3 IS-2 in design rules, simulations and safety margins. Knowing the idea lets you read a specification sheet and understand why the numbers look the way they do.
In the classroom
URMV-3 IS-2 is common in secondary-school and first-year university syllabi. It links to neighbouring topics 1950s Romanian sailplanes, Aircraft first flown in 1950, Glider aircraft, so understanding it makes those chapters shorter.
In everyday life
Look for URMV-3 IS-2 outside the textbook — in sport, cooking, traffic, electronics or the sky above you. An example you found yourself is remembered far longer than one you were given.
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How to study URMV-3 IS-2 in 20 minutes

  1. Read the reference excerpt below once, without taking notes.
  2. Close the page and write down what URMV-3 IS-2 means in your own words.
  3. Compare your version with the excerpt and mark what you missed.
  4. Work through the three examples above with pen and paper.
  5. Explain URMV-3 IS-2 out loud to somebody else — or to Teacher Smith in the lgStudy chat.

Frequently asked questions

What is URMV-3 IS-2 in simple terms?

The IS-2 was an intermediate training glider designed by Iosif Şilimon and built in Romania in the 1950s at the URMV-3 (Rom: Uzinele de Reparatii Material Volant-3 - Glider repair and manufacture factory) factory at Brașov. Design and development The IS-2 was designed as an intermediate training gl…

Why does URMV-3 IS-2 matter?

Because it connects several science ideas at once: it gives you a definition you can apply, a quantity you can calculate, and a way to check whether a result is plausible.

How should I study URMV-3 IS-2?

Read the excerpt, restate it from memory, then work through the examples and applications listed on this page. The five-step study plan above takes about twenty minutes.

What does this page cover?

It gives you a compact reference excerpt plus original lgStudy explanations, examples, applications and study material on URMV-3 IS-2.

Tags

  • 1950s Romanian sailplanes
  • Aircraft first flown in 1950
  • Glider aircraft
  • High-wing aircraft

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