Difference between revisions of "GDS.94 Flamingo"
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+ | {| border=0 cellspacing=0 cellpadding=4 style="float:right; margin:0 0 .5em 1em; width:250px; background:#fff; border-collapse:collapse; border:1px solid #999; font-size:85%; line-height:1.5; " | ||
+ | |- style="background:#f0f0f0; text-align:center; width=250px;" | ||
+ | | align=center colspan=2 |[[Image:UKIN_banner.gif|125px]] | ||
+ | |-style="background:#f0f0f0;" | ||
+ | | align=center colspan=2 | '''Profile (n/a)''' | ||
+ | |- style="text-align:center; background:#f0f0f0;" | ||
+ | | colspan=2 style="padding:0; background:#996; color:#fff;" | | ||
+ | |- style="color:#fff; background:#69c; font-size:140%;" | ||
+ | ! colspan=2 |Flamingo | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Design details | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Function | ||
+ | |Aerial decoy | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manufacturer | ||
+ | |[[Lyme and Martens Industries]] | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Design No. | ||
+ | |LM*- | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#41-60|GSI No.]] | ||
+ | |GDS.94 | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Unit cost | ||
+ | | | ||
+ | |-style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates | ||
+ | |[[Wikipedia:2004|2004]]-present | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |General characteristics | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Length | ||
+ | | m | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Diameter | ||
+ | | m | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Finspan | ||
+ | | m | ||
+ | |-style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Wingspan | ||
+ | | m | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Launch mass | ||
+ | | kg | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion | ||
+ | | | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control | ||
+ | |Tail control fins, thrust vectoring, extending wings | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | ||
+ | |[[Wikipedia:Mach|Mach]] 0.95 | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | ||
+ | |>6''[[Wikipedia:Acceleration_due_to_gravity|g]]'' | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Range | ||
+ | | | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling | ||
+ | | | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Guidance and payload | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Guidance | ||
+ | |[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system|INS]] with command uplink | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Payload | ||
+ | | | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Launch platforms | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Air force|Air]] | ||
+ | | | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Operators | ||
+ | |- | ||
+ | |colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]] | ||
+ | |} | ||
+ | |||
The '''GDS.94 Flamingo''' is a lightweight high-subsonic capable autonomous aerial decoy. It previously operated under the designations ALQ.220 and ADQ.220 before receiving its appropriate ADM designation, whereupon it was given a [[Defence Procurement Agency (Isselmere-Nieland)#Guided System Index|GSI number]]. | The '''GDS.94 Flamingo''' is a lightweight high-subsonic capable autonomous aerial decoy. It previously operated under the designations ALQ.220 and ADQ.220 before receiving its appropriate ADM designation, whereupon it was given a [[Defence Procurement Agency (Isselmere-Nieland)#Guided System Index|GSI number]]. | ||
Latest revision as of 02:56, 6 July 2007
Profile (n/a) | |
Flamingo | |
---|---|
Design details | |
Function | Aerial decoy |
Manufacturer | Lyme and Martens Industries |
Design No. | LM*- |
GSI No. | GDS.94 |
Unit cost | |
Service dates | 2004-present |
General characteristics | |
Length | m |
Diameter | m |
Finspan | m |
Wingspan | m |
Launch mass | kg |
Flight characteristics | |
Propulsion | |
Flight control | Tail control fins, thrust vectoring, extending wings |
Speed | Mach 0.95 |
Manoeuvrability | >6g |
Range | |
Ceiling | |
Guidance and payload | |
Guidance | GPS/INS with command uplink |
Payload | |
Launch platforms | |
Air | |
Operators | |
UKIN |
The GDS.94 Flamingo is a lightweight high-subsonic capable autonomous aerial decoy. It previously operated under the designations ALQ.220 and ADQ.220 before receiving its appropriate ADM designation, whereupon it was given a GSI number.
Topics on Isselmere-Nieland | ||
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