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Contents

   



(Top)
 


1 Overview  





2 Variants  





3 Specifications (Q-4/AQM-35A)  





4 See also  





5 References  














Northrop AQM-35: Difference between revisions






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Browse history interactively
 Previous edit
Content deleted Content added
Akradecki (talk | contribs)
24,127 edits
Changed designation from missle to UAV to conform to definitions being adopted in other articles
Sixshotkill (talk | contribs)
37 edits
 
(40 intermediate revisions by 23 users not shown)
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{{Short description|Supersonic drone}}

The '''AQM-35''' was a [[supersonic]] target [[Unmanned aerial vehicle|drone]] designed by the [[United States of America]].

{|{{Infobox aircraft begin

|name = Q-4 / AQM-35

|image = File:Northrop XQ-4 in flight.jpg

|caption = XQ-4

|alt =

}}{{Infobox aircraft type

|type = [[Target drone]]

|national origin = [[United States]]

|manufacturer = [[Northrop Corporation]]

|builder =

|designer =

|first flight = January 1956

|introduced =

|introdction =

|retired = mid 1960s

|status =

|primary user = [[United States Air Force]]

|more users =

|produced =

|number built = 25

|program cost =

|unit cost =

|developed from =

|variants with their own articles =

|developed into =

}}

|}


The '''AQM-35''' was a [[supersonic]] target [[Unmanned aerial vehicle|drone]] produced by the [[Northrop Corporation]].



==Overview==

==Overview==



The AQM-35 program began life in [[1953]] as the [[Northrop Corporation|Northrop]] Model RP-61 supersonic target drone. In June [[1954]] the [[United States Air Force]] awarded Northrop a contract for development of the project as the Q-4; the first flight-capable XQ-4 was launched in [[1956]].

The AQM-35 program began life in 1953 as the Model RP-61 supersonic target drone. In June 1954 the [[United States Air Force]] awarded Northrop a contract for development of the project as the Q-4; the first flight-capable XQ-4 was launched in 1956.



The XQ-4 was capable of either ground or air launch, though the former mode was never tested. It was powered by an [[Rolls-Royce Soar|XJ81-WE-3 ]][[turbojet]], allowing it to reach speeds of [[Mach number|Mach]] 1.55. The drone's course was followed with [[radar]], and flight commands were sent by a [[radio]] [[telemetry]] system. When the mission was completed the XQ-4 would deploy a three-stage [[parachute]] system along with four large inflatable airbags to cushion the impact with the ground.

The XQ-4 was capable of either ground or air launch, though the former mode was never tested. It was powered by a [[Rolls-Royce Soar|Westinghouse XJ81-WE-3]] [[turbojet]], allowing it to reach speeds of [[Mach number|Mach]] 1.55. The drone's course was followed with [[radar]], and flight commands were sent by a [[radio]] [[telemetry]] system. When the mission was completed the XQ-4 would deploy a three-stage [[parachute]] system along with four large inflatable airbags to cushion the impact with the ground.



The Air Force planned to use the Q-4 as a target for various [[Surface-to-air missile|surface-to-air]] and [[Air-to-air missile|air-to-air]] missiles. A secondary [[reconnaissance]] function was planned, with TV or cameras carried.

The Air Force planned to use the Q-4 as a target for various [[Surface-to-air missile|surface-to-air]] and [[Air-to-air missile|air-to-air]] missiles. A secondary [[reconnaissance]] function was planned, with TV or cameras carried. The drone was air-launched by a [[Lockheed DC-130|Lockheed DC-130 Hercules]] drone controller aircraft, or other carrier aircraft.



In[[1963]], the Q-4 family of drones were given the designation AQM-35A and AQM-35B. They were never considered entirely successful, with a variety of problems arising during both the development and flight testing phases. It was also considered that the flight performance of the drone was so high that it was not a realistic test for the missiles being developed - ironic since the whole point of the project was to develop a supersonic target. Only 25 of all types were ever built. The last examples of the type were retired during the 1960s.

In 1963, the Q-4 family of drones were given the designation AQM-35A and AQM-35B. They were never considered entirely successful, with a variety of problems arising during both the development and flight testing phases. It was also considered that the flight performance of the drone was so high that it was not a realistic test for the missiles being developed––ironic since the whole point of the project was to develop a supersonic target. Only 25 of all types were ever built. The last examples of the type were retired during the 1960s.



==Variants==

==Variants==

[[Image:Twuav 01 05.png|right]]

;XQ-4:Prototype of the RP-61 supersonic target drone.

;Q-4:Production target drones.

;Q-4A:Developed to use a [[Fairchild J83]] engine and a modified radar signature for testing the [[CIM-10 Bomarc]] missile. When the engine could not be developed in time the variant was cancelled.

;Q-4B: Fitted with a much more powerful [[General Electric J85|J85-GE-5]] engine and a strengthened airframe. This variant was first flown in 1961.

;AQM-35A:Post 1962 designation of the Q-4 drone.

;AQM-35B:Post 1962 designation of the Q-4B



==Specifications (Q-4/AQM-35A)==

The XQ-4A, was developed to use a have a [[Fairchild]] J83 engine and a modified radar signature for testing the CIM-10 Bomarc missile. When the engine could not be developed in time the variant was cancelled.

{{Aircraft specs


|ref=

In [[1959]] Northrop was given a contract to develop an improved Q-4B fitted with a much more powerful J85-GE-5 engine and a strengthened airframe. This variant was first flown in [[1961]].

|prime units?=kts


<!--

==Specifications==

General characteristics


-->

XQ-4/AQM-35A :

|length m=10.06


|length note=<br/>

*''Length'' : 10.06 m (33 ft)

::::'''Q-4B/AQM-35B:''' {{convert|35.333|ft|m|abbr=on|2}}

*''Wingspan'' : 3.38 m (11 ft 1 in)

|span m=3.38

*''Diameter'' : 51 cm (20 in)

|span note=<br/>

*''Height'' : 1.69 m (5 ft 7 in)

::::'''Q-4B/AQM-35B:''' {{convert| 12.666|ft|m|abbr=on|2}}

*''Weight'' : 900 kg (1,980 lb)

|height m=1.69

*''Speed'' : Mach 1.55

|height note=<br/>

*''Ceiling'' : 18,300 m (60,000 ft)

::::'''Q-4B/AQM-35B:''' {{convert| 6.167|ft|m|abbr=on|2}}

*''Propulsion'' : [[Rolls-Royce Soar|Westinghouse XJ81-WE-3]] turbojet, thrust 8.0 kN (1,810 lbf)

|dia m=0.51


|empty weight lb=1,980

XQ-4B/AQM-35B :

|empty weight note=<br/>


::::'''Q-4B/AQM-35B:''' {{convert| 3,400|lb|kg|abbr=on|0}}

*''Length'' : 10.77 m (35 ft 4 in)

<!--

*''Wingspan'' : 3.86 m (12 ft 8 in)

Powerplant

*''Diameter'' : 51 cm (20 in)

-->

*''Height'' : 1.88 m (6 ft 2 in)

|eng1 number=1

*''Weight'' : 1,540 kg (3,400 lb)

|eng1 name=[[Westinghouse XJ81-WE-3]]

*''Speed'' : Mach 2

|eng1 type=Lightweight expendable turbojet

*''Ceiling'' : 21,300 m (70,000 ft)

|eng1 lbf=1,810

*''Propulsion'' : General Electric J85-GE-5 turbojet, thrust 17.1 kN (3,850 lbf)

|eng1 note=<br/>


::::'''Q-4B/AQM-35B:''' 1x [[General Electric J85-GE-5]] turbojet, {{convert| 3,850|lbf|kN|abbr=on|0}} thrust

<!--

Performance

-->

|more performance=<br/>

*'''Maximum speed''': M1.55

::::'''Q-4B/AQM-35B:''' M2.0

|ceiling ft=60,000

|ceiling note=<br/>

::::'''Q-4B/AQM-35B:''' {{convert|70,000|ft|m|abbr=on|0}}

}}



==See also==

==See also==

{{aircontent|

|related=

|similar aircraft=

|lists=

|see also=

*[[List of missiles]]

*[[List of missiles]]

*[[Unmanned aerial vehicle]]

*[[Unmanned aerial vehicle]]

}}


==References==

{{commonscat}}

{{reflist}}

* [http://www.designation-systems.net/dusrm/m-35.html Northrop (Radioplane) Q-4/AQM-35]


{{Northrop aircraft}}

{{US missiles}}

{{US unmanned aircraft}}

{{USAF system codes}}



{{DEFAULTSORT:AQM-35}}

[[Category:UAVs and drones]]

[[Category:Unmanned vehicles]]

[[Category:Northrop aircraft|Q-004]]

[[Category:Modern missiles of the United States]]

[[Category:1950s United States special-purpose aircraft]]

[[Category:Target drones of the United States]]

[[Category:Single-engined jet aircraft]]

[[Category:High-wing aircraft]]


Latest revision as of 07:45, 15 May 2024

Q-4 / AQM-35
XQ-4
Role Target drone
National origin United States
Manufacturer Northrop Corporation
First flight January 1956
Retired mid 1960s
Primary user United States Air Force
Number built 25

The AQM-35 was a supersonic target drone produced by the Northrop Corporation.

Overview[edit]

The AQM-35 program began life in 1953 as the Model RP-61 supersonic target drone. In June 1954 the United States Air Force awarded Northrop a contract for development of the project as the Q-4; the first flight-capable XQ-4 was launched in 1956.

The XQ-4 was capable of either ground or air launch, though the former mode was never tested. It was powered by a Westinghouse XJ81-WE-3 turbojet, allowing it to reach speeds of Mach 1.55. The drone's course was followed with radar, and flight commands were sent by a radio telemetry system. When the mission was completed the XQ-4 would deploy a three-stage parachute system along with four large inflatable airbags to cushion the impact with the ground.

The Air Force planned to use the Q-4 as a target for various surface-to-air and air-to-air missiles. A secondary reconnaissance function was planned, with TV or cameras carried. The drone was air-launched by a Lockheed DC-130 Hercules drone controller aircraft, or other carrier aircraft.

In 1963, the Q-4 family of drones were given the designation AQM-35A and AQM-35B. They were never considered entirely successful, with a variety of problems arising during both the development and flight testing phases. It was also considered that the flight performance of the drone was so high that it was not a realistic test for the missiles being developed––ironic since the whole point of the project was to develop a supersonic target. Only 25 of all types were ever built. The last examples of the type were retired during the 1960s.

Variants[edit]

XQ-4
Prototype of the RP-61 supersonic target drone.
Q-4
Production target drones.
Q-4A
Developed to use a Fairchild J83 engine and a modified radar signature for testing the CIM-10 Bomarc missile. When the engine could not be developed in time the variant was cancelled.
Q-4B
Fitted with a much more powerful J85-GE-5 engine and a strengthened airframe. This variant was first flown in 1961.
AQM-35A
Post 1962 designation of the Q-4 drone.
AQM-35B
Post 1962 designation of the Q-4B

Specifications (Q-4/AQM-35A)[edit]

General characteristics

Q-4B/AQM-35B: 35.333 ft (10.77 m)
Q-4B/AQM-35B: 12.666 ft (3.86 m)
Q-4B/AQM-35B: 6.167 ft (1.88 m)
Q-4B/AQM-35B: 3,400 lb (1,542 kg)
Q-4B/AQM-35B: 1x General Electric J85-GE-5 turbojet, 3,850 lbf (17 kN) thrust

Performance

Q-4B/AQM-35B: 70,000 ft (21,336 m)
Q-4B/AQM-35B: M2.0

See also[edit]

References[edit]


Retrieved from "https://en.wikipedia.org/w/index.php?title=Northrop_AQM-35&oldid=1223935253"

Categories: 
Northrop aircraft
1950s United States special-purpose aircraft
Target drones of the United States
Single-engined jet aircraft
High-wing aircraft
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This page was last edited on 15 May 2024, at 07:45 (UTC).

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