umwelt-online: Bekanntmachung der vorläufigen Berechnungsverfahren für den Umgebungslärm nach § 5 Abs. 1 der Verordnung über die Lärmkartierung (34. BImSchV) (6)

Flugzeugklasse S 3.1a - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1800	0	80	0
4300	0	80	-
4800	-	80	460
5300	-3	80	-
9000	-3	80	920
20000	-3	135	1470
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 20000	0	0	0,05

Flugzeugklasse S 3.1b - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	45	0
3200	0	90	0
7300	0	90	-
7800	-	90	460
8300	-3	90	-
15600	-3	90	920
24600	-3	135	1190
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 24600	0	0	0,03

Flugzeugklasse S 3.1a/b - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7400	0	67	-
8400	-2,5	82	-
X	-2,5	98	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ ⋅ cot w - 300

h₀ 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 3.2a - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
3200	0	90	0
7300	0	90	-
7800	-	90	460
8300	-3	90	-
15600	-3	90	920
24600	-3	135	1525
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 21100	0	0	0,055

Flugzeugklasse S 3.2b - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	45	0
3300	0	90	0
7700	0	90	-
8200	-	90	460
8700	-3	90	-
17100	-3	90	920
26100	-3	135	1190
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 26100	0	0	0,03

Flugzeugklasse S 3.2a/b - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7400	0	67	-
8400	-2,5	82	-
X	-2,5	98	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ × cot w - 300

h₀ 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 4a - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
1700	0	90	0
4700	0	90	-
5200	-	90	460
5700	-1,5	90	-
10400	-1,5	90	920
21400	-1,5	135	1250
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 21400	0	0	0,03

Flugzeugklasse S 4b - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
2700	0	90	0
7600	0	90	-
8100	-	90	460
8600	-1,5	90	-
17100	-1,5	90	920
26100	-1,5	135	1190
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 26100	0	0	0,03

Flugzeugklasse S 4 a/b - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7400	0	67	-
8400	-3,5	82	-
X	-3,5	98	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ × cot w - 300

h₀ 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 s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1100	0	75	0
5100	0	75	-
5600	-	75	460
6100	-1	-	-
10400	-1	110	650
15000	-1	135	1000
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 15000	0	0	0,126

Flugzeugklasse S 5.1 - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	65	0
7400	0	65	-
X	-1	108	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ × cot w - 300

h₀ 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 s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1900	0	80	0
4100	0	80	-
4600	-	80	460
5100	-3	-	-
9000	-3	115	690
15300	-3	135	1200
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 15300	0	0	0,113

Flugzeugklasse S 5.2 - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
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

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	70	0
7400	0	75	-
X	-1	108	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ × cot w - 300

h₀ 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 5.3 - Ab

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
1	89,0	1,0
2	93,0	1,0
3	93,5	1,0
4	92,0	1,0
5	89,0	1,0
6	85,5	1,0
7	78,5	1,0
8	70,0	1,0

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
2000	0	85	0
4400	0	85	-
4900	-	85	460
5400	-2	-	-
8100	-2	115	610
11600	-2	135	830
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> 11600	0	0	0,117

Flugzeugklasse S 5.3 - An

Datenblatt s₀ = 300 m

n	(1) O_n [dB]	(2) R_n
1	72,5	1,0
2	76,5	1,0
3	77,0	1,0
4	75,5	1,0
5	72,5	1,0
6	69,0	1,0
7	62,0	1,0
8	53,5	1,0

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	68	0
7400	0	72	-
X	-1	108	h₀
σ' [m]	dZ/dσ' [dB/m	dV/dσ' [s^-1]	dM/dσ'
> X	0	0	0

X = h₀ × cot w - 300

h₀ 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

weiter