Research Article

Conceptual Design of a Small Hybrid Unmanned Aircraft System

Table 7

Lifting properties of He in standard (ISA) operating conditions.

Pressure altitude Air or helium temperature
Helium expected gross static lift
kg per kg of He
Helium density Air density

717.10456.780.16811.2241
1017.08506.780.16811.2238
1317.06556.780.16811.2234
1617.04606.780.16821.2231
1917.02656.780.16821.2227