Analysis of the Magnus Moment Aerodynamic Characteristics of Rotating Missiles at High Altitudes

Table 1

Variation of parameters with altitude.

Altitude (km)	Temperature (K)	Pressure (Pa)
0	289.10	101325	1.7940
2	276.44	78535	1.7323
4	263.79	60990	1.6694
6	251.13	46780	1.6050
8	238.48	35391	1.5391
10	226.15	26370	1.4733
12	221.46	19415	1.4479
14	221.50	14265	1.4481
16	221.50	10481	1.4481
18	221.50	7700	1.4481
20	221.50	5657	1.4481
30	226.51	1211	1.4753
40	250.33	286	1.6008
60	247.06	21	1.5839