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Flugzeugklasse P 1.3 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 79,5 1,0
2 78,5 1,0
3 74,0 1,0
4 70,0 1,0
5 65,0 1,0
6 59,0 1,0
7 52,0 1,0
8 44,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 18 0
250 0 36 0
X 0 36 ho
X + 1.000 -8 43 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X + 1.000 0 0 0

X = ho / 0,105 + 250

ho Flughöhe nach Nr. 2.2.1.4 bzw. Nr. 2.2.3.5 VBUF-DES

Flugzeugklasse P 1.3 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 69,5 1,0
2 68,5 1,0
3 64,0 1,0
4 60,0 1,0
5 55,0 1,0
6 49,0 1,0
7 42,0 1,0
8 34,0 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 150 0 31 0
X - 1.000 0 31 -
X 2 43 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 150

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 P 1.4 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 84,5 1,0
2 83,0 1,0
3 81,0 1,0
4 78,5 1,0
5 73,5 1,0
6 67,5 1,0
7 60,5 1,0
8 52,5 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 35 0
550 0 68 0
X 0 68 ho
X + 1.000 -5 75 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X + 1000 0 0 0

X = ho / 0,141 + 550

ho Flughöhe nach Nr. 2.2.1.4 bzw. Nr. 2.2.3.5 VBUF-DES

Flugzeugklasse P 1.4 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 77,5 1,0
2 76,0 1,0
3 74,0 1,0
4 71,5 1,0
5 66,5 1,0
6 60,5 1,0
7 53,5 1,0
8 45,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 51 0
X - 1 000 0 51 -
X 2 75 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 P 2.1 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 87,0 1,0
2 85,5 1,0
3 81,5 1,0
4 77,0 1,0
5 73,5 1,0
6 69,5 1,0
7 69,5 1,0
8 64,5 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 35 0
900 0 70 0
3.800 0 70 -
4.300 - 70 310
4.800 -2 70 340
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 4.800 0 0 0,06

Flugzeugklasse P 2.1 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 77,5 1,0
2 72,0 1,0
3 73,5 1,0
4 74,5 1,0
5 71,0 1,0
6 69,5 1,0
7 71,5 1,0
8 60,5 1,0

so=300m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 60 0
X - 1 000 0 60 -
X 5 70 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 P 2.2 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 94,5 1,0
2 93,0 1,0
3 89,0 1,0
4 84,5 1,0
5 81,0 1,0
6 77,0 1,0
7 77,0 1,0
8 72,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 35 0
900 0 70 0
3.800 0 70 -
4.300 - 70 310
4.800 -2 70 340
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 4.800 0 0 0.06

Flugzeugklasse P 2.2 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 77,5 1,0
2 72,0 1,0
3 73,5 1,0
4 74,5 1,0
5 71,0 1,0
6 69,5 1,0
7 71,5 1,0
8 60,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 60 0
X - 1.000 0 60 -
X 5 70 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 1.0 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 82,0 1,0
2 85,5 1,0
3 83,5 1,0
4 82,0 1,0
5 79,0 1,0
6 76,0 1,0
7 73,0 1,0
8 63,5 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 1.0 - 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=300m

(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 1.1 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 94,0 1,2
2 100,5 1,2
3 100,5 1,2
4 98,5 1,2
5 95,5 1,1
6 91,5 1,0
7 87,5 1,0
8 72,0 1,0

so - 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 40 0
1.300 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 1.1 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 76,0 1,2
2 78,5 1,2
3 80,0 1,2
4 78,0 1,2
5 75,5 1,1
6 77,0 1,0
7 77,5 1,0
8 65,0 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 1.2 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 94,0 1,2
2 100,5 1,2
3 100,5 1,2
4 98,5 1,2
5 95,5 1,1
6 91,5 1,0
7 87,5 1,0
8 72,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 40 0
1.400 0 80 0
3.100 0 80 -
3.600 - 80 460
4.100 -3 80 -
6.700 -3 80 920
12.300 -3 135 1120
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 12.300 0 0 0,13

Flugzeugklasse S 1.2 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 75,5 1,2
2 78,0 1,2
3 79,5 1,2
4 77,5 1,2
5 75,0 1,1
6 76,5 1,0
7 77,0 1,0
8 64,5 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 67 -
9.300 -2 67 -
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 1.3 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 96,0 1,2
2 102,5 1,2
3 102,5 1,2
4 100,5 1,2
5 97,5 1,1
6 93,5 1,0
7 89,5 1,0
8 74,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 3 40 0
1.900 0 80 0
4.400 0 80 -
4.900 - 80 460
5.400 - 3 80 -
9.600 - 3 80 920
13.000 - 3 110 990
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 13.000 0 0 0,12

Flugzeugklasse S 1.3 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 - 77,0 1,2
2 79,5 1,2
3 81,0 1,2
4 79,0 1,2
5 76,5 1,1
6 78,0 1,0
7 78,5 1,0
8 66,0 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 67 -
9.300 -2 67 -
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

UWS Umweltmanagement GmbH . Frame öffnen