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Flugzeugklasse S 2 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 95,5 1,2
2 102,0 1,2
3 102,0 1,2
4 100,0 1,2
5 97,0 1,1
6 93,0 1,0
7 89,0 1,0
8 73,5 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 40 0
1.300 0 80 0
3.600 0 80 -
4.100 - 80 460
4.600 - 3 80 -
7.800 - 3 80 920
18.800 - 3 135 1.283
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 18.800 0 0 0,033

Flugzeugklasse S 2 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 81,0 1,2
2 83,5 1,2
3 85,0 1,2
4 83,0 1,2
5 80,5 1,1
6 82,0 1,0
7 82,5 1,0
8 70,0 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 67 0
7.400 0 67 -
8.400 -2 82 -
X -2 98 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 3.1 a) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 93,0 1,2
2 94,0 1,2
3 94,0 1,2
4 92,0 1,2
5 92,0 1,1
6 91,0 1,0
7 86,0 1,0
8 73,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.800 0 80 0
4.300 0 80 -
4.800 - 80 460
5.300 -3 80 -
9.000 -3 80 920
20.000 -3 135 1.470
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 20.000 0 0 0,05

Flugzeugklasse S 3.1 b) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 93,0 1,2
2 94,0 1,2
3 94,0 1,2
4 92,0 1,2
5 92,0 1,1
6 91,0 1,0
7 86,0 1,0
8 73,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 45 0
3.200 0 90 0
7.300 0 90 -
7.800 - 90 460
8.300 -3 90 -
15.600 -3 90 920
24.600 -3 135 1.190
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 24.600 0 0 0,03

Flugzeugklasse S 3.1 a/b) - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 83,0 1,2
2 85,0 1,2
3 82,0 1,2
4 82,5 1,2
5 83,0 1,1
6 78,5 1,0
7 80,5 1,0
8 68,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
-300 0 67 0
7.400 0 67 -
8.400 -2,5 82 -
X -2,5 98 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 3.2 a) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 96,0 1,2
2 97,0 1,2
3 97,0 1,2
4 95,0 1,2
5 95,0 1,1
6 94,0 1,0
7 89,0 1,0
8 76,0 1,0

so=300m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.900 0 80 0
4.700 0 80 -
5.200 - 80 460
5.700 - 3 80 -
10.100 - 3 80 920
21.100 - 3 135 1.525
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 21.100 0 0 0,055

Flugzeugklasse S 3.2 b) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 96,0 1,2
2 97,0 1,2
3 97,0 1,2
4 95,0 1,2
5 95,0 1,1
6 94,0 1,0
7 89,0 1,0
8 76,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 45 0
3.300 0 90 0
7.700 0 90 -
8.200 - 90 460
8.700 -3 90 -
17.100 -3 90 920
26.100 -3 135 1.190
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 26.100 0 0 0,03

Flugzeugklasse S 3.2 a/b) - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 83,0 1,2
2 85,0 1,2
3 82,0 1,2
4 82,5 1,2
5 83,0 1,1
6 78,5 1,0
7 80,5 1,0
8 68,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
-300 0 67 0
7.400 0 67 -
8.400 -2,5 82 -
X -2,5 98 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 4 a) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 98,0 1,2
2 106,0 1,2
3 102,0 1,2
4 100,0 1,2
5 97,0 1,1
6 93,5 1,0
7 96,0 1,0
8 83,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 40 0
1.700 0 80 0
4.700 0 80 -
5.200 - 80 460
5.700 -1,5 80 -
10.400 -1,5 80 920
21.400 -1,5 135 1.250
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 21.400 0 0 0,03

Flugzeugklasse S 4 b) - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 98,0 1,2
2 106,0 1,2
3 102,0 1,2
4 100,0 1,2
5 97,0 1,1
6 93,5 1,0
7 96,0 1,0
8 83,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 45 0
2.700 0 90 0
7.600 0 90 -
8.100 - 90 460
8.600 -1,5 90 -
17.100 -1,5 90 920
26.100 -1,5 135 1.190
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 26.100 0 0 0,03

Flugzeugklasse S 4 a/b) - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 81,5 1,2
2 85,5 1,2
3 82,5 1,2
4 82,5 1,2
5 82,0 1,1
6 91,5 1,0
7 89,0 1,0
8 77,0 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 67 0
7.400 0 67 -
8.400 - 3,5 82 -
X - 3,5 98 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 5.1 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 78,0 1,0
2 81,5 1,0
3 79,5 1,0
4 78,0 1,0
5 75,0 1,0
6 72,0 1,0
7 69,0 1,0
8 59,5 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.100 0 75 0
5.100 0 75 -
5.600 - 75 460
6.100 -1 - -
10.400 -1 110 650
15.000 -1 135 1.000
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 15.000 0 0 0,126

Flugzeugklasse S 5.1 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 65,0 1,0
2 73,0 1,0
3 71,0 1,0
4 72,0 1,0
5 69,5 1,0
6 66,5 1,0
7 67,0 1,0
8 53,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 65 0
7.400 0 65 -
X - 1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 5.2 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 86,0 1,0
2 89,5 1,0
3 87,5 1,0
4 86,0 1,0
5 83,0 1,0
6 80,0 1,0
7 77,0 1,0
8 67,5 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.900 0 80 0
4.100 0 80 -
4.600 - 80 460
5.100 -3 - -
9.000 -3 115 690
15.300 -3 135 1.200
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ" dH/dσ"
> 15.300 0 [s-1] 0,113

Flugzeugklasse S 5.2 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 68,0 1,0
2 76,0 1,0
3 74,0 1,0
4 75,0 1,0
5 72,5 1,0
6 69,5 1,0
7 70,0 1,0
8 56,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
-300 0 70 0
7 400 0 75 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ'
>X 0 0 0

X = ho · cot w - 300

ho Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

UWS Umweltmanagement GmbH . Frame öffnen