





This
menu: Click on each country will give a detailed
history of each Sagitta ever registered in that country. Click on
"Brochure" will show original brochures and more
historic literature |
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"It is possible to fly without motors, but
not without knowledge and skill" - Wilbur Wright
Dutch sailplane factory: NV Vliegtuigbouw.
NV Vliegtuigbouw was started by Mr. A.L.
Bauling, the promotor of Aeroclub Teuge, when he realised that pilots in
Holland needed more Baby's and he saw an opportunity to build several 10's
of them. Production started in 1936 under supervision of Mr. Wijkens in an
attick, later in a large shed. After production was well going on they hired
Mr. Snellen as designer to build the -at that time- very modern V-20.
Unfortunately only one was ever built, see picture. If anyone has any pictures or more
information regarding this one, please contact us. The V-20 featured a
robust Göppingen 535
profile for the wing, wich was attached to the fuselage with struts. Stall
speed was 45 km/h (24 knots) and best glide angle (L/D) was 1:23. Very good
indeed in the era of Olympia's. Besides the V-20 they also built a
two-seater Grunau-8 and a trainer glider of type "Universal". Baby's however
always stayed the main production line. In total 16 Baby's where delivered
to Dutch gliding clubs. These Baby's are often called Bauling Baby's. They
have a larger and different shaped rudder than Fokker Baby's and other ones.
After WW2 they started again, this time based at Teuge airfield, with a
series of high performance gliders, the Sagitta. (source
www.grunaubaby.nl)

Interesting is that in 1952 the at that
time 17 year old Ed van Bree flew Bauling Baby PH-45 from Heerlen to
Langewiese, a distance of 176 km. Ed would later
become an important ambassador for the Sagitta, flying many displays with
the fully aerobatic Sagitta, often inverted a few metres above the deck. It
must have been an impressive sight, as these displays were still in memory
of the webmaster when he purchased his own Sagitta almost 40 years later... Ed
participated in the world champs 1963 in Argentina and competed with the
Sagitta against 22 K-6's, Foka-4, Edelweiss, Vasama and other hot
ships of those days. He gave an impressive display both at the opening day and last day of
the world championships and ended up 31st place. This picture shows Ed on
the right, with Jan Selen in the cockpit (uncle of -many many years later-
world champion Baer Selen). More exclusive images from 1963 on the
(Dutch) photogallery pages, and more about the championships, including
complete article from "Avia" on the
Argentine 1963 pages.
Piet Alsema and the Sagitta.
Little is known about designer
engineer Piet Alsema, here pictured in the cockpit of PH-280 (thank
you Erica Alsema, for the confirmation). Piet passed away in 1971. At the design stage of the
Sagitta he was
general manager of NV Vliegtuigbouw and three years of planning and design
cumulated in what
was
supposed to be one of the world's best gliders in the standard class
(restricted to 15 metres span). It turned out to become one of the last
wooden high performance gliders, before glassfibre as a construction
material took over completely. It also turned out to be the only high
performance single seat glider design ever to be series produced in Holland.
Besides sleek lines which made it a good looking machine, it had some very
modern features and an unusual airbrake design. The pin to lock both
tailplane halves together hides in the tailfin. The canopy has a 360 degrees
view and slides open backwards. It can be flown open in several fixed
positions. The wheel has a brake. All controls connect automatically upon
assembly (although this is not without danger - care should be taken that
the levers slide rightly into the forks when the
wings are mounted to the fuselage).
The first prototype, registered PH-266,
was flown by Mr. Bauling on the 4th of June or the 4th of July
1960, and the first production model, named Sagitta 2 and registered PH-280,
stood finished 24 November 1961. In 1964 a 17 metre version, the Super
Sagitta, was build on request of a Belgian pilot.
Only one was ever built, and it was later exported to the USA.

This picture, kindly borrowed from the
website of the Amsterdam Gliding Club (ACvZ), shows Piet Alsema second from
left. It was taken by Len Bosman shortly after WW2 with Prince Bernhard seen at the right
in the cockpit of a Goevier that survived the war. Instructor is Jan
Vastenau.
Below Piet Alsema is seen
at the tail of a Fieseler Storch borrowed from the prince and used as a
towplane the same day.

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Piet inspecting the wreck of a Grunau Baby
and already making plans with Jan Bosman how to rebuild it (it was flying
again within a year). Thanks for these pictures to Len Bosman, who together
with his brother Jan were more or less the official photographers of the
Amsterdam Gliding Club in the 40's. Click the pictures for a larger image.
And this is what it was all about: prototype Sagitta,
s/n 001, here on display in one of the very few colour pictures
ever: (Published with kind permission of Ken Elliott,
UK)

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A recent photo of the
birthplace of all Sagitta's, taken at Teuge airfield. This is the original
factory where all Sagitta's were built. The shed is beautifully restored and
is now in use as workshop for the Gliding Club Teuge. Click picture for more
images. Thanks Charles, and thanks to Teuge's technician who took the
pictures.
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A bit more about the
Standard Class. Source:
Zweefvliegen II from Wim Adriaansen, The Netherlands
The standard class was created out of the
need for affordable and simple gliders, that could be used for both competition
and club flying. The idea for this class was born at the
Organisation Scientifique et Technique Internationale du Vol a Voile, in
short OSTIV. This organisation handles all sorts of technical issues, and
one of them was to define the specifications for the standard class, started
in 1956. Up to 1956 all championships were flown in single seat or two seat
classes. The standard class was first flown in 1958. The goal was to
stimulate design of cheap and safe gliders, cheap to repair as well - and
thus stimulate gliding all over the world. Here are some of the
specifications:
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The maximum wing span is limited to 15
metres. |  |
Flaps and other means to change
the wing profile during flight are prohibited. |  |
The glider has to be equiped with a
fixed, non-retractable wheel. |  |
Ballast that can be ejected during
flight is prohibited. |  |
Brake parachutes are not allowed. |  |
The glider needs to be equiped with
dive brakes capable of limiting the maximum speed to Vne. |
After each world gliding championships
the OSTIV-award will be presented to the design that best meets these
criteria. This happened first time ever in Poland in 1958, when Alexander
Schleicher received the award for the Ka-6. In 1960 it was awarded for the
Standard Austria and later on for the Finnish PIK-16 Vasama. Competing
gliders from that time were Foka, Ka-6, Sagitta, Austria, the Australian
ES-59 Arrow, EON 460 and many others. According to Harrie Wiertz (technician
and crew of the Dutch team in Argentinia; he died in 1984) failing to win the OSTIV award was
due to sanding the wings wet, causing all surfaces to buckle in the burning
Argentine sun. The paint coatings were already way too thin, and the water
definitly ruined it. It wasn't a nice sight and one of the biggest disappointments in his life.
(source Harrie Wiertz jr.)
Standard Class in comparison:
| |
Ka-6 |
Austria |
Vasama |
Sagitta |
Foka |
EON-460 |
M-100-S |
Arrow |
| Wing span
(m) |
15 |
15 |
15 |
15 |
15 |
15 |
15 |
13.3 |
| Length (m) |
6.7 |
6.2 |
6.0 |
6.5 |
7 |
6.3 |
6.4 |
6.8 |
| Wing ratio |
18.1 |
16.7 |
19.2 |
18.7 |
18.5 |
20.2 |
17.1 |
16.0 |
| Wing area
(m²) |
12.4 |
13.5 |
11.7 |
12 |
12.2 |
11.2 |
13.1 |
11.0 |
| Wing
loading (kg/m²) |
24.2 |
24.0 |
22.5 |
26.7 |
25.7 |
24.4 |
24.0 |
25.5 |
| Weight
(kg) |
182 |
205 |
166 |
217 |
225 |
159 |
198 |
170 |
| Max load
(kg) |
115 |
118 |
115 |
110 |
87 |
113 |
117 |
110 |
| Vne (km/h) |
200 |
209 |
250 |
270 |
260 |
216 |
230 |
238 |
| Vmax rough
air (km/h) |
130 |
- |
170 |
200 |
160 |
144 |
140 |
139 |
| Min sink @
(km/h) |
68 |
68 |
73 |
78 |
75 |
70 |
67 |
68 |
| Vstall
(km/h) |
60 |
67 |
62 |
66 |
62 |
61 |
51 |
60 |
| LD |
31.5 |
34 |
34 |
33 |
34 |
30 |
32 |
28 |
| @ V (km/h) |
- |
105 |
85 |
85 |
86 |
- |
80 |
76 |
| First flight |
1955 |
1959 |
1961 |
1960 |
1960 |
1960 |
1960 |
1962 |
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Sagitta, Sagitta
2, Sagitta 013 and Super Sagitta.
Source: bits & pieces from Charles Munnig Schmidt and Louis
van Rijn, "Sport in de Luchtvaart"
1966 by Wim Adriaansen.
It is clear that a lot of things changed
from prototype (s/n 001, registration PH-266) to the serial produced glider. The first serial built Sagitta was
called Sagitta 2
(s/n 002, registration PH-280). All Sagittas after s/n 013 are called Sagitta 013, because
it was only then the Sagitta was fully certified. The Sagitta has always
been a heavy glider, due to the fact that it is build according to the very
strict Dutch airworthiness requirements; probably the most demanding in the
world. The wing spars are
build up of solid spruce and both wings and fuselage are covered with birch triplex. At one stage, probably
after test flights, the wing tip profile was changed from NACA63-618 (over the whole wing)
to NACA-4412, in order to make the tips stall later than the rest of the
wing and thus keeping aileron control longer. We know now that this wasn't
too successful. One other change was in shape and construction of the
canopy. Sagitta 001 is the only one with the very long nose, which makes it
really different from the rest. However, we don't know more than what we can see on the pictures
that are available. The prototype also had tailplanes that folded upwards for
transportation. This explains maybe why the tailplane can be hard to get
rigged on the later versions (with a main pin through the tail fin); it was
simply never designed like that originally. With the modification of the
tailplane also the shape and size of the rudder changed significantly. See
picture galleries and note the difference between s/n 001 and all other
Sagitta's. The wings connected to the
fuselage automatically with a sort of fork construction. Some other
details about the prototype are to be found in this
article (thanks Howard
Petri). Howard also submitted one of the
original advertisements drawings featuring the Sagitta logo, as depicted
on the tail of N6446, and an
article from Air
Progress 1964 - containing a seldom
seen picture of Piet Alsema. Original commercial brochures are to be
downloaded here.
British article:
Drawings:
Air Progress 1964: Brochure:
Development and design ideas.
Ongoing research in this area. We're
waiting on contributions from key people. The wing profile NACA 63-618 is
also used in the Ka-6 and Ka-6CR (root section), the Foka and Foka-5,
Schweizer 1-29 and the T-37 and T-45 (Skylark and Swallow). More info about
the wing profiles on the "technical" pages, with a contribution of Louis van
Rijn.
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