To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

INTA HM.1
An HM. 1 at the Museo del Aire, Cuatro Vientos, Madrid.
Role Primary trainer
National origin Spain
Manufacturer Aeronáutica Industrial S.A.
Designer Pedro Huarte-Mendicoa
First flight 1943
Number built 200

The INTA HM.1, also known as Huarte Mendicoa HM-1, was a 1940s Spanish primary trainer designed by the Instituto Nacional de Técnica Aeronáutica (INTA) and built for them by Aeronáutica Industrial S.A. (AISA).[1]

YouTube Encyclopedic

  • 1/3
    Views:
    163 403
    295 540
    311 857
  • Instagram me story kaise dalte hain | how to share story on instagram in hindi1
  • Wassanaya by Rathna Sri Wijesinghe-for GCE O/L students | ඔය දෑල දොඩමලුය : වස්සානය Grade 10/11
  • Indian History | Medieval Indian History | Shivaji Maharaj | Ramesh G | Sadhana Academy| Shikaripura

Transcription

Development

The HM.1 was designed by INTA as a two-seat primary training monoplane with a fixed tailwheel landing gear.[1] It was followed by a number of similar aircraft with equipment and accommodation changes.[1] The last of the family was the HM.7 built in 1947 which was an enlarged four-seat version powered by a 240 hp (179 kW) Argus As 10C engine, the HM.7 was the last powered aircraft designed by the Institute.[1]

Variants

HM.1
Two-seat primary trainer
HM.2
enclosed-cabin version of the HM.1 with retractable landing gear.
HM.3
open-cockpit floatplane variant
HM.5
single-seat advanced trainer
HM.7
enlarged four-seat version
HM.9
two-seat glider tug

Operators

 Spain

Specification HM.1

Data from Jane's Fighting Aircraft of World War II[2]

General characteristics

  • Crew: 2
  • Length: 7.65 m (25 ft 0 in)
  • Wingspan: 9.65 m (31 ft 8 in)
  • Height: 2.20 m (7 ft 2.25 in)
  • Wing area: 14 m2 (150.6 sq ft)
  • Empty weight: 620 kg (1,364 lb)
  • Gross weight: 850 kg (1,870 lb)
  • Powerplant: 1 × Elizalde G-IV-B Tigre 4-cylinder four-cylinder linear motor , 110 kW (150 hp)

Performance

  • Maximum speed: 230 km/h (142.8 mph, 124.1 kn)
  • Cruise speed: 195 km/h (121 mph, 105 kn)
  • Endurance: 3 hours 30 minutes
  • Service ceiling: 5,000 m (16,400 ft)

References

Notes

  1. ^ a b c d Orbis 1985, p. 2195
  2. ^ Bridgman 1988, p. 156

Bibliography

  • Bridgman, Leonard (1988). Jane's Fighting Aircraft of World War II. New York: Crescent Books. ISBN 0-517-67964-7.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.

External links

This page was last edited on 4 October 2023, at 23:34
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.