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Avro 730 (R.156T / O.R.330)


High-Altitude Supersonic Reconnaissance Aircraft


United Kingdom | 1957



"The Avro 730 was drawn up during the early Cold War period to satisfy a British high-speed, high-altitude reconnaissance platform - it was cancelled in 1957."



Authored By: Staff Writer | Last Edited: 09/25/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.
At the close of World War 2 (1939-1945) in 1945, the primary threat to the West became the Soviet Union and this spurred the global airpowers of the day (the United States, Britain, and France) to concentrate on development of a new generation of warplanes centered around a jet propulsion scheme. Engineers went to work and devised a multitude of solutions, many of which were destined to fall to naught, while others began either instant classic or largely forgettable entries.

Britain's Royal Air Force (RAF) has made good on one aspect of their defense-building - the ncuelar-capable "V-bomber" force centered on the Avro Vulcan, the Handley Page Victor, and the Vickers Valliant. It was soon realized that the service was also in need of a high-performance, high-altitude, supersonic reconnaissance platform to size up enemy strength. This led to a new requirement centered on a radar-equipped, day/night, all-weather, high-speed, high-flying reconnaissance platform through Specification "R.156T".

The new requirement was established in 1954 and, the following year, no fewer than five British aero-concerns took part in supplying varied submissions. Basic requirements were laid out: an operating ceiling as high as 70,000 feet with Mach 2.5 speeds being possible - the aircraft would avoid enemy ground-based defenses and interceptors through high altitude operation and sheer speed. The Air Ministry looked to have the new design settled as soon as 1960.

Avro engineers penciled out a futuristic design built around the prospect of very-high-speeds with the minimum of generated drag. The resulting, finalized design took on a dart-like overall shape in which the front of the fuselage was detailed only by canard foreplanes and an embedded cockpit while the aft-section carried a single vertical tail fin and seated the mainplanes. The mainplanes were given sweepback only along their leading edges and, within each member, would be buried the powerplants. The engines were to be aspirated by cone-capped (two-stage shock) intakes (set ahead of the leading edge) and exhausted aft through conventional ports (aft of the trailing edge). An early design shape of 1955 carried the engines in nacelles at the wingtips but more or less maintained the same sleek design appearance. This approach was, however, abandoned. Wing-mounted engines were also championed from the outset for they supported maintenance access and outright unit replacement - the latter allowing the aircraft to feature any new, or different, propulsion scheme with little change to the overall airframe.

An unconventional four-legged undercarriage would be featured to allow for the needed ground-running - a single nose leg paired with a inline main leg, these supported by outriggers set near each engine nacelle.

The embedded cockpit meant that the pilot was not granted conventional vision from his position. Rather, he would operate the aircraft through a periscope-type arrangement which would have presented issues all its own and require specialized training.

Multiple engine fits were considered for the Model 730, numbering as few as four units and as many as sixteen total turbojets. The operating crew was to be two, three, or four personnel but would have included at least one pilot and one or two navigators. Throughout the development process, the target all-up weight remained 200,000lb of which half would have to be committed to the necessary fuel stores for feeding the thirsty engines.

Between the nose section and main landing gear legs would be housed the side-looking "Red Drover" X-band aerial radar unit - critical to the mission success of the aircraft. The Mach 2.5 requirement ensured that the aircraft would have to incorporate steel (honeycomb sandwich) into its design which proved complex when compared to alloys but necessary to combat heat generation at the speeds and operating altitudes required of the aircraft.

The finalized form of the Model 730, as submitted to Air Ministry authorities, incorporated 4 x Armstrong Siddeley P.159 afterburning turbojet engines of 20,750lb thrust coupled with 2 x Armstrong Siddeley rocket motors offering additional thrust only during take-off actions.

Avro engineers targeted a first-flight before the end of 1959 to which three more flyable examples would join the program the following year. From this work would be had production-quality forms for in-service testing to which formal adoption would have come in 1964 of thereabouts. However, cancellation of the project came in 1957 (by way of the infamous "Defence White Paper") when the first prototype was still under construction. It was perceived that advancements in Soviet air defenses would have negated any performance benefits of the Model 730 by the time it would have entered service. Additionally, British through turned towards a future battlefield owned by missiles.

Beyond a completed mockup, partial prototype, and some early wind tunnel testing completed, there was little to be shown for the funding, work, and time put into bringing the complex Avro 730 to fruition.

The Americans found greater success in development of their own high-altitude supersonic reconnaissance platform at about the same time, this becoming the Lockheed SR-71 "Blackbird" spyplane detailed elsewhere on this site.

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Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Avro 730 High-Altitude Supersonic Reconnaissance Aircraft.
4 x Armstrong Siddeley P.159 afterburning turbojet engines developing 20,750 lb of thrust; 2 x Armstrong Siddeley rocket motors for assisted take-off thrust.
Propulsion
1,920 mph
3,090 kph | 1,668 kts
Max Speed
60,039 ft
18,300 m | 11 miles
Service Ceiling
5,754 miles
9,260 km | 5,000 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Avro 730 High-Altitude Supersonic Reconnaissance Aircraft.
2
(MANNED)
Crew
163.4 ft
49.80 m
O/A Length
59.7 ft
(18.20 m)
O/A Width
222,667 lb
(101,000 kg)
MTOW
Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.
RANGE
ALT
SPEED
Armament
Available supported armament and special-mission equipment featured in the design of the Avro 730 (R.156T / O.R.330) High-Altitude Supersonic Reconnaissance Aircraft .
None. Mission equipment centered on photographic reconnaissance systems.
Variants
Notable series variants as part of the Avro 730 (R.156T / O.R.330) family line.
Model 730 - Base Project Designation.
Operators
Global customers who have evaluated and/or operated the Avro 730 (R.156T / O.R.330). Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 0 Units

Contractor(s): Avro Aircraft (A.V. Roe) - UK
National flag of the United Kingdom

[ United Kingdom (cancelled) ]
Relative Max Speed
Hi: 2000mph
Lo: 1000mph
Aircraft Max Listed Speed (1,920mph).

Graph Average of 1,500 MPH.
Era Crossover
Pie graph section
Showcasing Aircraft Era Crossover (if any)
Max Alt Visualization
Small airplane graphic
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Aviation Timeline
EarlyYrs
WWI
Interwar
WWII
ColdWar
Postwar
Modern
Future
1 / 1
Image of the Avro 730 (R.156T / O.R.330)
Image copyright www.MilitaryFactory.com; No Reproduction Permitted.

Mission Roles
Some designs are single-minded in their approach while others offer a more versatile solution to airborne requirements.
RECONNAISSANCE
X-PLANE
Recognition
Some designs stand the test of time while others are doomed to never advance beyond the drawing board; let history be their judge.
Going Further...
The Avro 730 (R.156T / O.R.330) High-Altitude Supersonic Reconnaissance Aircraft appears in the following collections:
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