TY - GEN
T1 - Preliminary design and cost analysis of a family of unmanned aerial vehicles
AU - Zych, Thomas
AU - Selig, Michael S.
N1 - Publisher Copyright:
© 1995 American Institute of Aeronautics and Astronautics. All Rights Reserved.
PY - 1995
Y1 - 1995
N2 - This paper summarizes the results of a study on the design of high altitude long endurance (HALE) unmanned aerial vehicles (TJAVs). A review of previous designs revealed that most were point- designs rather than general purpose vehicles, leading to cost inefficiencies. It was therefore determined that efforts should be made to design HALE UAVs that are capable of performing a wide variety of missions. Additionally, it is desirable for these vehicles to be as inexpensive as possible, in order to allow their use by a wider base of customers. In the present study, a family of three mission-configurable HALE vehicles has been designed. Between them, these vehicles span the majority of the payload/endurance requirements of previous designs. In addition, through the use of common parts and subassemblies among the three craft, it is shown that vehicle unit cost can be reduced substantially; perhaps by as much as 25%.
AB - This paper summarizes the results of a study on the design of high altitude long endurance (HALE) unmanned aerial vehicles (TJAVs). A review of previous designs revealed that most were point- designs rather than general purpose vehicles, leading to cost inefficiencies. It was therefore determined that efforts should be made to design HALE UAVs that are capable of performing a wide variety of missions. Additionally, it is desirable for these vehicles to be as inexpensive as possible, in order to allow their use by a wider base of customers. In the present study, a family of three mission-configurable HALE vehicles has been designed. Between them, these vehicles span the majority of the payload/endurance requirements of previous designs. In addition, through the use of common parts and subassemblies among the three craft, it is shown that vehicle unit cost can be reduced substantially; perhaps by as much as 25%.
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M3 - Conference contribution
AN - SCOPUS:84963795133
SN - 9781563471230
T3 - 13th Applied Aerodynamics Conference
SP - 977
EP - 985
BT - 13th Applied Aerodynamics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 13th Applied Aerodynamics Conference, 1995
Y2 - 19 June 1995 through 22 June 1995
ER -