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CarboEurope R.E. Project Scientific Objectives Workpackage description Experiment plan 2005 Campaign 2007 Campaign CarboEurope R.E. data Information Upload site 2005 data access 2007 data access Partners Working papers News Join the mailing list Contact us ![]() |
III.2.5.1 EquipmentMetAir's "Dimona HB-2335" is both an advanced, and ecologically sound airborne measuring platform. It is a two seated, self-launching powered glider (Dimona HK-36 TTC ECO) silent, low fuel consumption, but 150...200 km/h cruising speed / 5 h endurance. Underwing-pods with two times 50 kg for equipment (scientific instruments) contain state of the art sensors for meteorology, and chemistry, position, 3-d-wind, temperature, dewpoint, in turbulent resolution (10 Hz), for eddy fluxes with H2O, CO2, CO, NO2, heat and momentum.The MetAir standard equipment includes sensors for:
figure III.2.5.1-a: The Dimona at Saucats airland during the COCA 2001 campaign. III.2.5.2 Flight plansDimona will contribute to 5 to 6 days of measurements, with one or two flights per day (3 to 4.5 hours each). With two flights per day, they will be from about 9 to 12 h, and 14 to 18 h LT, or with one extended flight per day between 11 and 16 h LT. In the following, the basic flight pattern is discussed with different aspects on different graphics. figure III.2.5.2-a: MetAir's basic flight legs MA1 through MA5 shown together with the existing design of the pattern "Landes" for the Aztec MA1 is the ferry flight to some "center point,
MA2+MA3 are the transsect for westerly winds, and MA2+MA4 for southwesterly
winds. They are not not necessarily flown
together with the Aztec, but, taking the same tracks might ease the permission,
and there might be occasions, where the flights are quasi-synchronous.
The same is true for the leg MA1, which is on one of the "SkyArrow
tracks" (not shown here).
However, in contrast to Aztec and SkyArrows which
fly on different constant altitudes, our task can only be fulfilled, when we
can change altitude on these legs between near surface (minimum save flight
altitude, see below), and about 2500 m AMSL (8000 ft) quite frequently. The
ascents will be made in 8-shaped turns perpendicular to the wind, with the
turns against the wind (see details on the last figure below). Then, we descend to the lowest point of the
next profile. The separation between the profiles is depending from the wind
speed. We try to move with the air mass (lagrangian measurement). Since ascents
are made with about 2 to 3 m/s vertical speed (130 km/h horizontal speed), and
descents with about –4 m/s (200 km/h), one ascent/descent cycle over 2500 m
takes about half an hour. With an average wind speed of 10 m/s (20 kt or 36
km/h) in the boundary layer, this would result in distances between profiles of about 20 km (or less with
lower wind speed as in figure III.2.5.2-d). Also the top of the profiles
could be adjusted according to the actual height of the boundary layer.
Especially during flights before noon, 1500 m MSL might be enough. Considering the limitations of the air spaces with
their complex vertical structure and temporal activity (see figure III.2.5.2-c),
not every profile might be possible to the desired altitude at any time.
However, we hope, that for the benefit of the project, most will be possible.
Before each ascent, we will request the clearance from the relevant ATC. It is
no problem to wait a few minutes when the actual traffic situation does not
allow to continue, but, it's possible later (a delay or a divert to another
position is less a problem than a "no go"). Our altitude is always
visible on the radars, since we have Transponder-C, which is encoding height.
Perhaps it would be practical, when we could get a "squawk"
(transponder code) for each active measuring day, or even for the campaign?
When flying from LFCS via WP1
to the coast, we will fly on constant altitude about 300 m GND (which is
about on 1000 ft MSL). In principle, each of these legs could be flown on this
altitude for flights in parallel with the SkyArrows, or for transfers. The dark blue air spaces on the bottom graph are
Aquitaine TMA Sectors 2 and 4 (class D and E), and the red ones are all special
use (restricted) air spaces from Cazaux, Biscarosse, Landes West, Captieux,
Mont-de-Marsan. We will have to find out, under what conditions we will be allowed
to enter them. The blue flight tracks on the map are as in figure III.2.5.2-a
(MA1 to MA5). In the vertical cross section (bottom graph), the black track is
the upper envelope (top of the profiles). We do not know yet, if MA3
will be possible (the leg from WP1 in figure III.2.5.2-c to the east, and back to WP3),
because it crosses several restricted air spaces (see also figure III.2.5.2-d).
Especially during days with southwesterly
winds, MA4 (from WP1 to the NE) might be an alternative which crosses less
restricted air spaces. However, for wind directions between 260 and 300°,
it would be most desirable to use MA3. figure III.2.5.2-d: details of the pattern for westerly winds (MA2+MA3) On this map, more details of the pattern for
westerly winds (MA2+MA3) are shown, together with a better identification of
the air spaces. The cross-legs (short north-south-legs of 3 to 5 km length) are
the vertical profiles as discussed with figure
III.2.5.2-b,
with an average horizontal separation of 15 km in this example (suitable for a
wind speed of about 30 km/h). These cross legs will be flown as 8-shaped
ascending "zig-zag" perpendicular to the wind, with all the turns
against the wind (this is to avoid crossing the own exhaust gases which could
happen when circling).
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