Saab 210

Saab 210
Χώρα	Σουηδία
Ρόλο	Πειραματικά αεροσκάφη
Πρώτη πτήση	21 Ιανουαρίου 1952
Χτισμένο	1

Teh Σάαμπ 210 Ντράκεν (ο Δράκος ή ο Χαρταετός) είναι ένα κλιμακωτό πεδίο δοκιμών για την ιδέα του διπλού δέλτα στην ανάπτυξη του μαχητικού J 35. Αν και ποτέ δεν ονομάστηκε επίσημα τίποτα άλλο εκτός από το Draken από τον Saab, σύντομα έγινε γνωστό με το ανεπίσημο ψευδώνυμό του Lilldraken (ο Μικρός Δράκος ή ο Μικρός Χαρταετός) μετά την πρώτη πτήση του πρωτοτύπου του Saab 35. Η πρώτη του πτήση ήταν στις 21 Ιανουαρίου 1952.

Πηγή: Saab 210 στη Βικιπαίδεια

SAAB 210 Lilldraken Walk Around
Photographer	Unknow
Localisation	Unknow
Photos	29

SAAB 210 Lilldraken 01

SAAB 210 Lilldraken 02

SAAB 210 Lilldraken 03

SAAB 210 Lilldraken 04

SAAB 210 Lilldraken 05

SAAB 210 Lilldraken 06

SAAB 210 Lilldraken 07

SAAB 210 Lilldraken 08

SAAB 210 Lilldraken 09

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General Characteristics and Role

The SAAB 210 Lilldraken (“Little Dragon”) was a revolutionary Swedish experimental aircraft designed and built by Saab in the early 1950s. It was created purely as a one-third scale research platform to test the novel and complex double delta wing configuration proposed for the supersonic Saab 35 Draken fighter. The Lilldraken was a critical step in the Draken’s development, as the double delta design—characterized by a small, highly-swept inner delta wing and a larger, less-swept outer delta—was entirely new and its aerodynamic properties needed real-world validation, especially at low speeds. Its unique profile and small size made it one of the most distinctive and important experimental aircraft of its era.

Property	Typical Value (SAAB 210)
Ρόλο	Experimental/Aerodynamic Testbed
National Origin	Σουηδία
Κατασκευαστής	Saab AB
First Flight	21 Ιανουαρίου 1952
Πλήρωμα	1 (Pilot)
Διαμόρφωση	Low-wing monoplane, double delta wing, tricycle landing gear
Μήκος	6.1 m (20 ft 0 in)
Εκπέτασμα	4.79 m (15 ft 8 in)
Max Speed	Approx. 340 km/h (211 mph)

Design Innovations and Performance

Engine: 1 x Armstrong Siddeley Adder turbojet engine (non-afterburning).
Thrust: Approx. 475 kgf (1,047 lbf).
Key Innovation: The primary purpose was to test the double delta wing, which was necessary to give the subsequent Draken fighter both high-speed performance (via the inner delta) and low-speed stability (via the outer delta).
Air Intakes: The Lilldraken featured large lateral air intakes on either side of the cockpit, which were also representative of the intended design for the larger Draken.
Test Program: The aircraft successfully performed numerous flights, validating the stability, control, and general handling characteristics of the radical double delta configuration before the full-scale fighter was finalized.

Legacy and Final Status

Successor: The knowledge gained from the Lilldraken program was directly applied to the full-scale development and successful deployment of the Mach 2-capable Saab 35 Draken fighter.
Operational Status: Only one example of the SAAB 210 was ever built.
Preservation: The single prototype is now preserved and displayed at the Flygvapenmuseum (Swedish Air Force Museum) in Linköping, Sweden.