013 Sagitta | |
---|---|
Role | Standard-class sailplane |
National origin | Netherlands |
Manufacturer | N.V. Vliegtuigbouw |
Designer | Piet Alsema |
First flight | 4 July 1960 [1] |
Status | Production completed |
Number built | 20 |
The N.V. Vliegtuigbouw 013 Sagitta (English: Arrow) is a Dutch mid-wing, single-seat Standard Class glider designed by Piet Alsema and produced by N.V. Vliegtuigbouw. [2] [3] [4] [5]
The aircraft is reported by different sources under a variety of different names and designations. Sources label it the Alsema Sagitta, Vliegtuigbouw Sagitta, N.V. Vliegtuigbouw 013 Sagitta, Dutch Sagitta, N.V. Vliegtuigbouw Sagitta 013 and N.V. Vliegtuigbouw Sagitta-013. The US type certificate erroneously lists it as the N.V. VLIEGTUIGBOUW Segitta (sic) 013 and catalogs it in their database under Vilegtuigbouw (sic), N.V., 013. [2] [3] [4] [5]
The Sagitta was designed by Alsema between 1957-61 specifically for the then-new FAI Standard Class. Like other early standard class gliders it was quickly surpassed in performance by newer fibreglass aircraft. [2] [3]
The Sagitta has a wooden structure. The fuselage is covered with plywood, the wings and tail surfaces with plywood and doped aircraft fabric covering. The 15.0 m (49.2 ft) span wing features top and bottom air brakes and employs NACA 63-618 airfoil at the wing root, and a NACA 4412 section at the wing tip. The controls are automatically connected on assembly. The bubble canopy slides aft for cockpit access and can be locked open in several positions in flight. The landing gear is a fixed monowheel. [2] [3] [6]
In the Netherlands the aircraft was certified for cloud flying and aerobatics, but its US certification does not include these authorizations. The type received its US type certificate on 2 August 1965. [2] [3] [4]
In July 2011 six Sagittas were still registered with the US Federal Aviation Administration. [5]
Data from Sailplane Directory, Soaring and FAA type certificate G7eu [2] [3] [4] The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II [1]
General characteristics
Performance
Aircraft of comparable role, configuration, and era
Related lists
{{cite web}}
: CS1 maint: year (link)The Aer-Pegaso M-100 was a single-seat glider designed and built in Italy from 1957.
The Schweizer SGS 2-32 is an American two-seat, mid-wing, two or three-place glider built by Schweizer Aircraft of Elmira, New York.
The Slingsby T.49 Capstan is a British two-seat glider of the 1960s built by Slingsby Sailplanes as a replacement for their earlier Type 42 Eagle.
The SZD-20x Wampir II was a single-seat tail-less research glider designed and built in Poland from 1959.
The Standard Austria was a single-seat aerobatic glider that was originally designed and built in Austria from 1959 but production was moved in 1962 to Schempp-Hirth in Germany.
The IS-4 Jastrząb was a single-seat aerobatic glider designed and built in Poland from 1949.
The Slingsby Type 45 Swallow was designed as a club sailplane of reasonable performance and price. One of the most successful of Slingsby's gliders in sales terms, over 100 had been built when production was ended by a 1968 factory fire.
The Neiva BN-1 was a high performance single seat sailplane designed in Brazil in the 1950s. It had national records, competition success, and went into production for club use.
The Schreder Airmate HP-8 is an American, high-wing single seat glider that was designed by Richard Schreder after the loss of the HP-7 in 1957.
The Johnson RHJ-6 Adastra was an American mid-wing, two-seat glider that was designed and constructed by Dick Johnson and first flown on 3 April 1960.
The Matteson M-1 was an American high-wing, single-seat, FAI Open Class glider that was designed and built by Fred Matteson of Palo Alto, California and Alfred Vogt of Schempp-Hirth.
The Hütter Hü 17, is a German high-wing, strut-braced, single-seat, utility training glider that was designed by brothers Ulrich Hütter and Wolfgang Hütter in the 1930s.
The Vogt Lo-150 is a West German high-wing, single seat glider that was designed by Alfred Vogt and produced by the Wolf Hirth Company.
The Lehtovaara PIK-16 Vasama is a Finnish mid-wing, single-seat, FAI Standard Class glider that was designed by Tuomo Tervo, Jorma Jalkanen and Kurt Hedstrom, who were students at the Polyteknikkojen Ilmailukerho (PIK) and produced by Lehtovaara.
The Scheibe Zugvogel is a West German, high-wing, single-seat, FAI Open Class glider that was produced by Scheibe Flugzeugbau. The first version was designed by Rudolph Kaiser and subsequent versions by Egon Scheibe.
The Schleicher Ka-4 Rhönlerche II, sometimes called the KA-4 or even K 4, is a West German high-wing, strut-braced, two-seat glider that was designed by Rudolf Kaiser and produced by Alexander Schleicher GmbH & Co.
The Schleicher K7 Rhönadler is a West German high-wing, two-seat, glider that was designed by Rudolf Kaiser and produced by Alexander Schleicher GmbH & Co.
The Brochocki BKB-1 was a Canadian mid-wing, single-seat, experimental tailless glider that was designed and constructed by Stefan Brochocki with assistance from Witold Kasper and A. Bodek. The designation indicated the contributions of all three men. The aircraft was intended to study flight above the stall angle.
The Antonov A-15 is a Soviet mid-wing, V-tailed single-seat, FAI Open Class glider that was designed by Oleg Antonov and produced by Antonov.
The Wassmer WA-30 Bijave is a French two-seat advanced training glider designed and built by Wassmer Aviation of Issoire.