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DTIC-AD-P010756

  • Version
  • 184 Downloads
  • 1.11 MB File Size
  • 1 File Count
  • March 5, 2017 Create Date
  • March 5, 2017 Last Updated
Scroll for Details

Design and Airworthiness Requirements for Military Unmanned Air Vehicle Systems

This paper examines the safety implications and factors 
to be considered for the procurement of a UAV and 
identifies the design requirements to be used as a guide 
to produce an air vehicle specification. It will touch on 
matters covered in more detail by other presenters 
because of the need to reflect the information they 
provide within the new standard. It should be noted that 
while appreciating that dirigibles and micro UAV's will 
be introduced in the filture, it was agreed that the current 
UK Defence Standard 00-970 should comply with 
current policy agreed within the United Kingdom (UK) 
Ministry of Defence (Mol)), and that by the Civil 
Aviation Authority (CAA), which is, that UAV Systems 
under 20kgs should be treated as models and as such do 
not need to comply with the regulations governing 
aircraft. This paper also identifies the role of the 
"Airworthiness, Design Requirements and Procedures 
(ADRP) organisation" of the UK MOD Defence 
Procurement Agency (DPA) and details the work being 
carried out in developing a set of general design and 
airworthiness requirements for UAV systems. ADRP are 
part of the new Defence Procurement Agency (DPA). 
which was formed on the I st of April 1999, to take 
forward the "SMART" Procurement initiative, which 
aims to use faster, cheaper and better ways of equipping 
the UK armed forces. This involves Integrated Project 
Teams (IPT) managing the programmes throughout the 
life of the equipment. This paper discusses the current 
and future UAV Systems requirements and gives a brief 
insight into the strategy adopted to produce a set of 
regulatory documents and procedures for the guidance of 
the MOD Integrated Project Team leader (IPT/L). This is 
done by ensuring adequate procedures are in place for 
the safe and airworthy operation of such aircraft. These 
procedures set the minimum standard required to 
accommodate the safe operation of all UAV systems in 
all airspace conditions subject to any limitations and 
constraints imposed by the design.

 

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DTIC-AD-P010756

  • Version
  • 184 Downloads
  • 1.11 MB File Size
  • 1 File Count
  • March 5, 2017 Create Date
  • March 5, 2017 Last Updated
Scroll for Details

Design and Airworthiness Requirements for Military Unmanned Air Vehicle Systems

This paper examines the safety implications and factors 
to be considered for the procurement of a UAV and 
identifies the design requirements to be used as a guide 
to produce an air vehicle specification. It will touch on 
matters covered in more detail by other presenters 
because of the need to reflect the information they 
provide within the new standard. It should be noted that 
while appreciating that dirigibles and micro UAV's will 
be introduced in the filture, it was agreed that the current 
UK Defence Standard 00-970 should comply with 
current policy agreed within the United Kingdom (UK) 
Ministry of Defence (Mol)), and that by the Civil 
Aviation Authority (CAA), which is, that UAV Systems 
under 20kgs should be treated as models and as such do 
not need to comply with the regulations governing 
aircraft. This paper also identifies the role of the 
"Airworthiness, Design Requirements and Procedures 
(ADRP) organisation" of the UK MOD Defence 
Procurement Agency (DPA) and details the work being 
carried out in developing a set of general design and 
airworthiness requirements for UAV systems. ADRP are 
part of the new Defence Procurement Agency (DPA). 
which was formed on the I st of April 1999, to take 
forward the "SMART" Procurement initiative, which 
aims to use faster, cheaper and better ways of equipping 
the UK armed forces. This involves Integrated Project 
Teams (IPT) managing the programmes throughout the 
life of the equipment. This paper discusses the current 
and future UAV Systems requirements and gives a brief 
insight into the strategy adopted to produce a set of 
regulatory documents and procedures for the guidance of 
the MOD Integrated Project Team leader (IPT/L). This is 
done by ensuring adequate procedures are in place for 
the safe and airworthy operation of such aircraft. These 
procedures set the minimum standard required to 
accommodate the safe operation of all UAV systems in 
all airspace conditions subject to any limitations and 
constraints imposed by the design.

 

FileAction
DTIC-AD-P010756 Design and Airworthiness Requirements for Military Unmanned Air Vehicle Systems.pdfDownload 
17,005 Documents in our Technical Library
2448873 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...