BAE Systems HERTI
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The BAE Systems HERTI is an unmanned aerial vehicle (UAV) developed by the British company BAE Systems. HERTI stands for High Endurance Rapid Technology Insertion and was developed in Warton United Kingdom. The HERTI airframe is based on a motor glider designed by Jaroslaw Janowski of J&AS Aero Design Poland. Its first flight was in December 2004 at the Australian Woomera test range where much of the test flight programme has been undertaken.

* Figure 3-55: BAE Systems Herti Next Generation Autonomous Air System * Table3-56: BAE Systems Herti Key Roles * 1
The BAE Systems Herti, based on a Polish motor-glider, first flew in 2004. It will weigh 750 kg, as built by Slingsby Aviation.2
BAE Systems HERTI Makes Far East Debut At LIMA 2007 3 Dec BAE Systems and Wipro Announce Aerospace Partnership 29 Nov www.baesystems.3
ZZ254 BAE Systems Herti UAV BAE Systems, Warton Notes: 1.4
BAE Systems Herti & Mantis Attached Thumbnails Attached ThumbnailsClick image for larger version. Name: BAE_Mantis2.jpg Views: 150 Size: 633.5

Made by BAE Systems.

BAE Systems Herti Next Generation Autonomous Air System Table3-18 3-31 BAE Systems Herti Key Roles Table 3-19 3-32 H 6
BAE Systems Herti Next Generation Autonomous Air System Table3-18 BAE Systems Herti Key Roles Table 3-19 H BAE Systems Herti Key Specifications 7
control, interesting to look at are the BAE Systems HERTI and Taranis UAVs: http://en.wikipedia.org/wiki/BAE_HERTI http://en.wikipedia.8
BAE Systems Herti Next Generation Autonomous Air System Table3-18 BAE Systems Herti Key Roles Table 3-19 H BAE Systems 9
Length Alt
500.38
Power Alt
100 hp
Loaded Weight Main
340.0
Introduction
2007
Payload Main
150.0
Cruise Speed Main
232.0
Ceiling Main
6
100 m
Type Of Prop
variable pitch propeller
Crew
none
Number Of Propellers Per Engine
1
Span Main
12 m
Cruise Speed Alt
8700.0
Jet Or Prop
prop
Primary user
Span Alt
1198.88
Plane Or Copter?
Avionics
Information and Exploitation Systems based on 3 x Radstone Computers
Engine(prop)
Rotax 914 4-cylinder horizontally opposed with
Propeller Or Rotor
propeller
Manufacturer
Payload Alt
330.0
First Flight
2004
Loaded Weight Alt
750.0
Power Main
75.0
Number Of Props
1
Length Main
5 m
Range Alt
72000.0
Ceiling Alt
20000.0
Category

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