Engineering:Composite Engineering BQM-167 Skeeter

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Short description: US Air Force aerial target drone
BQM-167 Skeeter
BQM-167 Skeeter target drone
Role Unmanned target drone
National origin United States
Manufacturer Composite Engineering Inc.
Kratos Defense & Security Solutions
Status In service
Primary user United States Air Force
Number built 37[1]
Developed into Kratos BQM-177[2]

The Composite Engineering BQM-167 Skeeter is a subscale aerial target (drone) developed and manufactured by Composite Engineering Inc. (acquired by Kratos Defense & Security Solutions) and operated by the United States Air Force and certain international customer air forces (designation BQM-167i). It replaced the Beechcraft MQM-107 Streaker.

Design and development

The BQM-167 was developed and manufactured by Composite Engineering Inc. (now part of Kratos Defense & Security Solutions), and is constructed of carbon fiber and epoxy-based materials.[1][3]

Two prototype targets were built and test flown in 2001. The BQM-167A was selected as the next-generation Air Force subscale aerial target in July 2002. A total of six targets were built for use during the flight performance demonstration (FPD) phase with its first flight 8 December 2004. A total of 13 FPD launches were made into March 2006.[1]

First acceptance testing was completed in August 2006, then pre-operational testing consisted of 13 test flights using production targets from August 2006 - June 2007. The first BQM-167 air-to-air missile live-fire mission took place 7 February 2007. Initial Operational Capability was achieved in 2008. Each target cost US$570,000.[1]

Operational history

BQM-167 being prepared for launch

The 82nd Aerial Targets Squadron operates and maintains the target at Tyndall Air Force Base, Florida.

The drone is land-launched using a rocket-assisted takeoff and launched from a rail system, and recovered on land or sea using a parachute system. After assessment and refurbishment, the drone is placed back into service.[1]

The USAF has had 37 in inventory.[1]

On 19 March 2021, a BQM-167 washed ashore in Boynton Beach, Florida after a weapon systems evaluation.[4]

Variants

UTAP-22 Mako

Launch of a UTAP-22 tactical unmanned vehicle in April 2021

On 23 November 2015, Kratos completed the second flight of its self-funded Unmanned Tactical Aerial Platform (UTAP-22), a development of the BQM-167A converted into a low-cost unmanned combat aerial vehicle (UCAV). The test involved collaborative airborne operations with a manned AV-8B Harrier fighter for 94 minutes demonstrating command and control through a tactical data-link, autonomous formation flying with the AV-8B, and transfer of UTAP-22 control between operators in a tactical network and then to an independent control link.[5] The 6.1 m (21 ft)-long turbojet-powered aircraft can travel at Mach 0.91 (693 mph; 1,115 km/h) up to an altitude of 50,000 ft (15,000 m) with a maximum range of 1,400 nmi (1,600 mi; 2,600 km) and an endurance of three hours. It can carry a 159 kg (351 lb) internal payload, a 227 kg (500 lb) external payload, and has a 45 kg (99 lb)-capable weapon hardpoint on each wing. The platform is recoverable on land or at sea using a parachute system.[6][7] In May 2017, the UTAP-22 received the official name Mako.[8] The aircraft costs between $2-$3 million.[9]

Operators

 United States
  • United States Air Force
SingaporeSingapore
  • Republic Of Singapore Air Force[10]
 Sweden
  • Swedish Defence Materiel Administration[11]

Specifications

Data from

Slovene pronunciation: [{{{1}}}]Thai pronunciation: [{{{1}}}]Neukirch, Jürgen; Schmidt, Alexander; Wingberg, Kay (2000), Cohomology of Number Fields, Grundlehren der Mathematischen Wissenschaften, 323, Berlin: Springer-Verlag, ISBN 978-3-540-66671-4 Template:ScribuntoPersian pronunciation: [{{{1}}}]{| class="wikitable" width="100%"

! rowspan="3" colspan="2" width="14%" style="border-bottom:2px solid grey;" | Date/Time (UTC) ! Configuration ! Serial number ! Launch site ! Outcome |-

|style="text-align:center;background-color:#e3e9e9;" | Payload |style="text-align:center;background-color:#e3e9e9;" | Separation orbit |style="text-align:center;background-color:#e3e9e9;" | Operator |style="text-align:center;background-color:#e3e9e9;" | Function |- | colspan="4" style="text-align:center;background-color:#e4dfdf;border-bottom:2px solid grey;" | Remarks |-

Parameter 1=time required!

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Chambers, Robert; Thomson, Thomas Napier (1857). "[[s:A biographical dictionary of eminent Scotsmen/|]]". A Biographical Dictionary of Eminent Scotsmen. Glasgow: Blackie and Son. {{{1}}}Polish pronunciation: [{{{1}}}]Malagasy pronunciation: [{{{1}}}]Japanese pronunciation: [{{{1}}}]Armenian pronunciation: [{{{1}}}]Czech pronunciation: [{{{1}}}]Manx pronunciation: [{{{1}}}]http://www.iucnredlist.org/apps/redlist/details/full/{{{1}}}/0 Alemannic German pronunciation: [{{{1}}}]Tagalog pronunciation: [{{{1}}}]Egyptian Arabic pronunciation: [{{{1}}}]French pronunciation: ​[{{{1}}}]Error: Invalid time.In progress In progressPalomares, M. L. D. and Pauly, D., eds. (2011). "{{{1}}} {{{2}}}" in SeaLifeBase. April 2011 version.Turkish pronunciation: [{{{1}}}]Finnish pronunciation: [{{{1}}}]Froese, Rainer and Pauly, Daniel, eds. (2006). "{{{1}}} {{{2}}}" in FishBase. April 2006 version.

|- | ... | — | — | — | — | — | —

|-Old Norse pronunciation: [{{{1}}}]Salish pronunciation: [{{{1}}}]Basque pronunciation: [{{{1}}}]{{{1}}}data-sort-value="" style="background: #ececec; color: #2C2C2C; vertical-align: middle; font-size: smaller; text-align: center; " class="table-na" | UnreleasedNorwegian pronunciation: [{{{1}}}] (aged {{{4}}})Hungarian pronunciation: [{{{1}}}]Quechua pronunciation: [{{{1}}}]Arabic pronunciation: [{{{1}}}]Punjabi pronunciation: [{{{1}}}]Afrikaans pronunciation: [{{{1}}}]Romanian pronunciation: [{{{1}}}]Hebrew pronunciation: [{{{1}}}][INVALID OR MISSING PARAMETER IN TEMPLATE Composite Engineering BQM-167 Skeeter]Uto-Aztecan pronunciation: [{{{1}}}]Tamil pronunciation: [{{{1}}}]Hindustani pronunciation: [{{{1}}}]Swedish pronunciation: [{{{1}}}]Kazakh pronunciation: [{{{1}}}]

Lao pronunciation: [{{{1}}}]Tibetan pronunciation: [{{{1}}}]Khmer pronunciation: [{{{1}}}]data-sort-value="" style="vertical-align:middle; text-align:center" class="table-na" | —{{{1}}}Welsh pronunciation: [{{{1}}}]Incomplete Partially doneAthabaskan pronunciation: [{{{1}}}]Māori pronunciation: [{{{1}}}]IPA: [{{{1}}}]Bulgarian pronunciation: [{{{1}}}]Korean pronunciation: [{{{1}}}]Icelandic pronunciation: ​[{{{1}}}]Sanskrit pronunciation: [{{{1}}}]Bengali pronunciation: [{{{1}}}]Indonesian pronunciation: [{{{1}}}]Serbo-Croatian pronunciation: [{{{1}}}]CROSBI {{{1}}}US Air Force - Fact Sheet, BQM-167A[1]

Slovene pronunciation: [{{{1}}}]Thai pronunciation: [{{{1}}}]Neukirch, Jürgen; Schmidt, Alexander; Wingberg, Kay (2000), Cohomology of Number Fields, Grundlehren der Mathematischen Wissenschaften, 323, Berlin: Springer-Verlag, ISBN 978-3-540-66671-4 Template:ScribuntoPersian pronunciation: [{{{1}}}]{| class="wikitable" width="100%"

! rowspan="3" colspan="2" width="14%" style="border-bottom:2px solid grey;" | Date/Time (UTC) ! Configuration ! Serial number ! Launch site ! Outcome |-

|style="text-align:center;background-color:#e3e9e9;" | Payload |style="text-align:center;background-color:#e3e9e9;" | Separation orbit |style="text-align:center;background-color:#e3e9e9;" | Operator |style="text-align:center;background-color:#e3e9e9;" | Function |- | colspan="4" style="text-align:center;background-color:#e4dfdf;border-bottom:2px solid grey;" | Remarks |-

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Chambers, Robert; Thomson, Thomas Napier (1857). "[[s:A biographical dictionary of eminent Scotsmen/|]]". A Biographical Dictionary of Eminent Scotsmen. Glasgow: Blackie and Son. {{{1}}}Polish pronunciation: [{{{1}}}]Malagasy pronunciation: [{{{1}}}]Japanese pronunciation: [{{{1}}}]Armenian pronunciation: [{{{1}}}]Czech pronunciation: [{{{1}}}]Manx pronunciation: [{{{1}}}]http://www.iucnredlist.org/apps/redlist/details/full/{{{1}}}/0 Alemannic German pronunciation: [{{{1}}}]Tagalog pronunciation: [{{{1}}}]Egyptian Arabic pronunciation: [{{{1}}}]French pronunciation: ​[{{{1}}}]Error: Invalid time.In progress In progressPalomares, M. L. D. and Pauly, D., eds. (2011). "{{{1}}} {{{2}}}" in SeaLifeBase. April 2011 version.Turkish pronunciation: [{{{1}}}]Finnish pronunciation: [{{{1}}}]Froese, Rainer and Pauly, Daniel, eds. (2006). "{{{1}}} {{{2}}}" in FishBase. April 2006 version.

|- | ... | — | — | — | — | — | —

|-Old Norse pronunciation: [{{{1}}}]Salish pronunciation: [{{{1}}}]Basque pronunciation: [{{{1}}}]{{{1}}}data-sort-value="" style="background: #ececec; color: #2C2C2C; vertical-align: middle; font-size: smaller; text-align: center; " class="table-na" | UnreleasedNorwegian pronunciation: [{{{1}}}] (aged {{{4}}})Hungarian pronunciation: [{{{1}}}]Quechua pronunciation: [{{{1}}}]Arabic pronunciation: [{{{1}}}]Punjabi pronunciation: [{{{1}}}]Afrikaans pronunciation: [{{{1}}}]Romanian pronunciation: [{{{1}}}]Hebrew pronunciation: [{{{1}}}][INVALID OR MISSING PARAMETER IN TEMPLATE Composite Engineering BQM-167 Skeeter]Uto-Aztecan pronunciation: [{{{1}}}]Tamil pronunciation: [{{{1}}}]Hindustani pronunciation: [{{{1}}}]Swedish pronunciation: [{{{1}}}]Kazakh pronunciation: [{{{1}}}]

Lao pronunciation: [{{{1}}}]Tibetan pronunciation: [{{{1}}}]Khmer pronunciation: [{{{1}}}]data-sort-value="" style="vertical-align:middle; text-align:center" class="table-na" | —{{{1}}}Welsh pronunciation: [{{{1}}}]Incomplete Partially doneAthabaskan pronunciation: [{{{1}}}]Māori pronunciation: [{{{1}}}]IPA: [{{{1}}}]Bulgarian pronunciation: [{{{1}}}]Korean pronunciation: [{{{1}}}]Icelandic pronunciation: ​[{{{1}}}]Sanskrit pronunciation: [{{{1}}}]Bengali pronunciation: [{{{1}}}]Indonesian pronunciation: [{{{1}}}]Serbo-Croatian pronunciation: [{{{1}}}]CROSBI {{{1}}}Kratos Unmanned Systems - Quick Facs, BQM-167A[12]

General characteristics

  • Crew: None
  • Length: 20 ft 0 in (6.1 m)
  • Wingspan: 10 ft 6 in (3.2 m)
  • Height: 4 ft 0 in (1.2 m)
  • Empty weight: 690 lb (313 kg)
  • Max takeoff weight: 2,050 lb (930 kg)
  • Powerplant: 1 × 1x MicroTurbo Tri 60-5+ turbojet, 990 lbf (4.4 kN) thrust

Performance

  • Maximum speed: 600 kn (690 mph, 1,100 km/h) (sea level)
  • Cruise speed: 230 kn (260 mph, 430 km/h) (sea level)
  • Service ceiling: 50,000 ft (15,000 m) MSL [clarification needed] 50 ft AGL min. / 8 m min.
    9 G turns; recovered by a parachute recovery system either from land or water

Avionics
IR and RF Tow Targets; IR and RF Wing Pods;[clarification needed] Chaff / Flare Dispensing; Vector & Scalar Scoring

References

Template:Kratos Defense