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Convair B-58A Hustler
USAF four-engine delta-wing supersonic strategic bomber, U.S.A.


Archive Photos 1


[1959 Convair B-58A "Hustler" (AF 59-2458, c/n 61) at the National Museum of the United States Air Force, WPAFB, Dayton, OH (Photos by John Shupek)]

Overview 2


  • Convair B-58 Hustler
  • Role: Supersonic strategic bomber
  • National origin: United States
  • Manufacturer: Convair
  • First flight: 11 November 1956
  • Introduction: 15 March 1960
  • Retired: 31 January 1970
  • Status: Retired
  • Primary user: United States Air Force
  • Number built: 116
  • Unit cost: US$12.44 million (equivalent to $80.26 million today)
  • Variants: Convair Model 58-9

The Convair B-58 Hustler was the first operational jet bomber capable of Mach 2 flight. The aircraft was designed by Convair and developed for the United States Air Force (USAF) for service in the Strategic Air Command (SAC) during the 1960s. It used a delta wing, which was also employed by Convair fighters such as the F-102, with four General Electric J79 engines in underwing pods; carried one nuclear weapon and fuel in a combination bomb/fuel pod under the fuselage, rather than in an internal bomb bay. Later on, four additional external hardpoints were added to allow five weapons to be carried.

Replacing the Boeing B-47 Stratojet strategic bomber, it was originally intended to fly at high altitudes and supersonic speeds to avoid Soviet fighters. The B-58 Hustler was notorious for its sonic boom, which was often heard by the public as it passed overhead in supersonic flight.

The introduction of highly-accurate Soviet surface-to-air missiles forced the B-58 into a low-level-penetration role that severely limited its range and strategic value, and it was never employed to deliver conventional bombs. This resulted in only a brief operational career between 1960 and 1970 when the B-58 was succeeded by the smaller, swing-wing FB-111A.

Design and Development 2


The genesis of the B-58 program was the Generalized Bomber Study (GEBO II) issued in February 1949 by the Air Research and Development Command (ARDC) at Wright-Patterson AFB, Ohio, for the development of a supersonic, long-range, bombardment aviation platform. The proposed bomber's design and development was to begin less than two years after sustained supersonic flight had been achieved. Contractors who bid to perform the generalized study (that hopefully would lead to a development contract) included Boeing, Convair, Curtiss, Douglas, Martin and North American Aviation.

Convair, which had built the XF-92A and other delta-wing fighters, initially looked at swept and semi-delta configurations, then settled on the delta wing planform, which offered good internal volume for support systems and fuel. It also had low wing loading (for airframe size), permitting supersonic flight in the mid-stratosphere at 50,000 to 70,000 ft (15,000 to 21,000 m). The final Convair proposal, coded FZP-110, was a radical two-place, delta wing bomber design powered by General Electric J53 engines. The performance estimates included a 1,000 mph (1,600 km/h) speed and a 3,000-mile (4,800 km) range.

The Air Force chose Boeing (MX-1712) and Convair MX-1626 to proceed to a Phase 1 study. The Convair design, refined and redesignated the MX-1964, was chosen in December 1952 to meet the newly proposed SAB-51 (Supersonic Aircraft Bomber) and SAR-51 (Supersonic Aircraft Reconnaissance), the first General Operational Requirement (GOR) worldwide for supersonic bombers. In February 1953, the Air Force issued a contract to develop Convair's design.

The resulting B-58 design was the first "true" USAF supersonic bomber program. The Convair design was based on a delta wing with a leading-edge sweep of 60° with four General Electric J79-GE-1 turbojet engines, capable of flying at Mach 2. Although its large wing made for relatively low wing loading, it proved to be surprisingly well suited for low-altitude, high-speed flight. It seated three (pilot, bombardier/navigator, and defensive systems operator) in separated tandem cockpits. Later versions gave each crew member a novel ejection capsule that could eject at an altitude of 70,000 ft (21,000 m) at speeds up to Mach 2. Unlike standard ejection seats of the period, a protective clamshell would enclose the seat and the control stick with an attached oxygen cylinder, allowing the pilot to continue to fly even "turtled up" and ready for immediate egress. The capsule was buoyant; the crewmember could open the clamshell, and use it as a life raft. Unusually, the ejection systems was tested with live bears and chimpanzees.[1] The XB-70 would use a similar system with capsules of a different design.

B-58 Crewmember Escape Capsule

To protect against the heat generated while cruising at Mach 2, the crew compartment, the wheel wells and electronics bay were pressurized and air conditioned. The B-58 was one of the first extensive applications of aluminum honeycomb panels, which bonded outer and inner aluminum skins to a honeycomb of aluminum or fiberglass.

The pilot's cockpit was rather conventional for a large multi-engine aircraft. The electronic controls were ambitious and advanced for the day. The navigator and DSO's cockpits featured wraparound dashboards with warning lights and buttons, and automatic voice messages and warnings from a tape system were audible through the helmet sets. Research during the era of all-male combat aircraft assignments revealed that a woman's voice was more likely to gain the attention of young men in distracting situations. Nortronics Division of Northrop Corporation selected actress and singer Joan Elms to record the automated voice warnings. To those flying the B-58, the voice was known as "Sexy Sally."

Weapons Systems

The Sperry AN/ASQ-42 bombing/navigation system combined a sophisticated inertial navigation system with the KS-39 Star tracker (astro-inertial navigation system) to provide heading reference, the AN/APN-113 Doppler radar to provide ground speed and wind speed data, a search radar to provide range data for bomb release and trajectory, and a radar altimeter. The AN/ASQ-42 was estimated to be 10 times more accurate than any previous bombing/navigation system.

Defensive armament consisted of a single 20 mm (0.79 in) T-171E-3 rotary cannon with 1,200 rounds of ammunition in a radar-aimed tail barbette. It was remotely controlled through the Emerson MD-7 automated radar fire-control system only requiring the DSO to lock-on a selected target blip on his scope and then fire the gun. The system computed aiming, velocity or heading differential, and range compensation. Offensive armament typically consisted of a single nuclear weapon, along with fuel tanks, in a streamlined MB-1C pod under the fuselage. Incurable difficulties with fuel leakage resulted in the replacement of the MB-1C with the TCP (Two Component Pod), which placed the nuclear weapon in an upper section while the lower fuel component could be independently jettisoned. This had the added benefit of allowing the pilot to "clean up" the aircraft for fuel efficiency or in case of emergency, while still retaining the (somewhat) slimmer weapon.

The first prototype, serial number 55-660, was completed in late August 1956. The first flight took place in November 1956. A difficult and protracted flight test program involving 30 aircraft continued until April 1959. The final B-58 was delivered in October 1962.

From 1961 to 1963, the B-58 was retrofitted with two tandem stub pylons under each wing root, adjacent to the centerline pod, for B43 or B61 nuclear weapons for a total of five nuclear weapons per aircraft. Although the USAF looked at using the B-58 for conventional strikes, it was never equipped for carrying or dropping conventional bombs. A photo reconnaissance pod, the LA-331, was also fielded. Several other specialized pods for ECM or an early cruise missile were considered, but not adopted. The late-1950s High Virgo air-launched ballistic missile was designed to be launched from the B-58; a Hustler carried out four test launches to determine ballistic missile and anti-satellite weapon system capability.

Operational History 2


The B-58 crews were chosen from other strategic bomber squadrons. Due to some characteristics of delta-winged aircraft, new pilots used the Convair F-102 Delta Dagger as a conversion trainer, before moving to the TB-58A trainer. The B-58 was difficult to fly and its three-man crews were constantly busy, but its performance was exceptional. A lightly loaded Hustler would climb at nearly 46,000 ft/min (235 m/s). In addition to its much smaller weapons load and more limited range than the Boeing B-52 Stratofortress, the B-58 had been extremely expensive to acquire.

Excessive Program Expenditure

Through FY 1961, the total cost of the B-58 program was $3 billion ($20 billion in 2018 dollars). A highly complex aircraft, it also required considerable maintenance, much of which required specialized equipment and ground personnel. For comparison, the average maintenance cost per flying hour for the B-47 was $361, for the B-52 it was $1,025 and for the B-58 it was $1,440. The B-58 cost three times as much to operate as the B-52. The cost of maintaining and operating the two operational B-58 wings (39 aircraft per wing) equaled that of six wings of B-52s (only 15 aircraft per wing). Because of the support costs of six wings vs only two wings, the actual cost per aircraft of the B-52s were $1.42 million per year vs $1.21 million per year for the B-58. (. This included special detailed maintenance for the nose landing gear, which retracted in a complex fashion to avoid the center payload. Compounding this, the B-58 had a high accident rate: 26 B-58 aircraft were lost in accidents, 22.4% of total production, more than half of the losses occurred during flight tests. The SAC senior leadership had been doubtful about the aircraft type from the beginning, although its crews eventually became enthusiastic about the aircraft. General Curtis LeMay was never satisfied with the bomber, and after a flight in one declared that it was too small, far too expensive to maintain in combat readiness and required an excessive number of aerial refuelings to complete a mission. Although the high altitude ferry range of the B-58 was better than that of the B-47's, the lack of forward basing resulted in a requirement for more KC-135 tanker support.

Adverse Flight Characteristics

While its performance and design were exceptional and appreciated, it was not easy to fly. This was caused by the 60° leading edge sweepback of its wing and was inherent in these types of delta wing platforms. It required a much higher angle of attack than a conventional aircraft, up to 9.4° at Mach 0.5 at low altitudes. If the angle of attack was too high, in excess of 17°, the bomber could pitch up and enter a spin. Several factors could prevent a successful recovery: if the pilot applied elevon, if the center of gravity was not correctly positioned, or if the spin occurred below 15,000 feet (4,600 meters), recovery might not be possible. The B-58 also had stall characteristics that were unconventional. If the nose was elevated, the bomber maintained forward motion without pitching down. Unless large amounts of power were applied, the descent rate increased rapidly. Another problem pilots faced was called "fuel stacking" and took place when the B-58 accelerated or decelerated. It was due to fuel moving in the tanks and causing sudden changes in the center of gravity. This could cause the aircraft to pitch or bank and subsequently lose control. The B-58 was very difficult to safely recover from the loss of an engine at supersonic cruise due to differential thrust. For this reason a system was retrofitted which would retard the symmetrical outboard engine automatically in the event of the failure of an outboard engine at high Mach numbers (above Mach 1.2) without any pilot action being required.

The aircraft had unusual takeoff requirements, with a 14° angle of attack needed for the rotation at about 203.5 knots (376.9 km/h; 234.2 mph) for a 150,000-pound (68,000 kg) combat weight. This poor takeoff performance was evident with the high landing speed, necessitating a drogue parachute for braking, which was also required for B-47 and B-52 aircraft.

Operational Wings and Retirement

Two SAC bomb wings operated the B-58 during its operational service: the 43d Bombardment Wing (which later transitioned to the 43rd Airlift Wing), based at Carswell AFB, Texas from 1960 to 1964, and Little Rock AFB, Arkansas from 1964 to 1970; and the 305th Bombardment Wing, based at Bunker Hill AFB (later Grissom AFB), Indiana from 1961 to 1970. The 305th also operated the B-58 combat crew training school (CCTS), the predecessor of the USAF's current formal training units (FTUs).

By the time the early problems had largely been resolved and SAC interest in the bomber had solidified, Secretary of Defense Robert McNamara decided that the B-58 was not a viable weapon system. It was during the B-58's introduction that high-altitude Soviet surface-to-air missiles (SAM) became a threat, especially the SA-2 Guideline, a SAM system the Soviet Union extensively deployed. The "solution" to this problem was to fly at low altitudes, minimizing the radar line-of-sight and reducing exposure time.

Because of dense air at low altitudes, the B-58 could not fly at supersonic speeds and its moderate range was reduced further, negating the costly high-speed performance of the design. In late 1965, Secretary McNamara ordered retirement of the B-58 by 1970. Despite efforts of the Air Force to earn a reprieve, the phase out proceeded on schedule. The last B-58s were retired in January 1970 and placed in storage with the Military Aircraft Storage and Disposition Center (MASDC) at Davis-Monthan Air Force Base. The fleet survived until 1977, when nearly all remaining aircraft were sold to Southwestern Alloys for disposal. The B-58 as a weapons system was replaced by the FB-111A. This was designed for low-altitude attack, to be more flexible with the carriage of conventional weapons, and less expensive to produce and maintain.

A total of 116 B-58s were produced: 30 trial aircraft and 86 production B-58A models. Most of the trial aircraft were later upgraded to operational standard. Eight were equipped as TB-58A training aircraft.

Since B-58 pilots were the only USAF pilots experienced in long-duration supersonic flight, several former Hustler crew members were selected by Colonel Douglas Nelson to fly the Lockheed SR-71 Blackbird at the start of that program.

Test Aircraft

A number of B-58s were used for special trials. One was specially modified to test the Hughes radar system intended for the Lockheed YF-12 interceptor and the North American F-108 Rapier, which had an extended nose to accommodate the radar and was nicknamed "Snoopy". Several improved (and usually enlarged) variants, named B-58B and B-58C by the manufacturer, were proposed but never built.

World Records

The B-58 set 19 world speed records, including coast-to-coast records, and the longest supersonic flight in history. In 1963, it flew from Tokyo to London (via Alaska), a distance of 8,028 miles (12,920 km) in 8 hours, 35 minutes, 20.4 seconds, averaging 938 miles per hour (1,510 kilometres per hour). As of 2016, this record still stands. The aircraft was serving in an operational unit, and had not been modified in any way besides being washed and waxed. One of the goals of the flight was to push the limit of its new honeycomb construction technique. The speed of the flight was limited only by the speed at which they believed the honeycomb panels would delaminate, although one of the afterburners malfunctioned and the last hour of the flight was continued at subsonic speed. This reduced the average speed to roughly Mach 1.5, despite most of the flight being at Mach 2. This B-58 was called "Greased Lightning" – the codename for the record attempt.

Some of the record winning aerospace trophies the B-58 won were the Blériot trophy, the Thompson trophy, the Mackay trophy, the Bendix trophy and the Harmon trophy.

Variants 2


  • XB-58: Prototype; two built.
  • YB-58A: Pre-production aircraft; 11 built.
  • B-58A: Three-seat medium-range strategic bomber aircraft; 86 built.
  • TB-58A: Training aircraft. Eight conversions from YB-58A.
  • NB-58A: This designation was given to a YB-58A used to test the General Electric J93 engine, originally intended for the North American XB-70 Valkyrie Mach 3 bomber.
  • RB-58A: Variant with ventral reconnaissance pod; 17 built.
  • B-58B: Unbuilt. Larger and faster than the B-58A, this version would have had uprated J79-GE-9 engines, a longer fuselage for extra fuel capacity, canards, and the ability to carry conventional weapons. A prototype B-58B was ordered (S/N 60-1109) and a total purchase of 185 envisioned, but the entire project was canceled before construction began, due to budgetary considerations. The B variant was also planned to be the mothership for a Mach 4 parasite called the FISH, for First Invisible Super Hustler. That FISH had three ramjets that would be ignited at an altitude of at least 35,000 feet (11,000 meters) and speeds over Mach 2. The Super Hustler would then drop from the B-58B, climb to 90,000 feet (27,000 meters), and accelerate to Mach 4.2 to complete its mission.
  • B-58C: Unbuilt. Proposed as a cheaper alternative to the XB-70, this enlarged version would have carried more fuel and 32,500 lbf (145 kN) J58 engines, the same ones used on the Lockheed SR-71. Design studies were conducted with two- and four-engine designs. Capable of carrying conventional weapons, the C model had an estimated top speed approaching Mach 3, a supercruise capability of about Mach 2, a service ceiling of about 70,000 ft (21,300 m), and a maximum range of 5,200 nautical miles (6,000 mi; 9,600 km). As enemy defenses against high-speed, high-altitude penetration bombers improved, the value of the B-58C diminished and the program was canceled in early 1961.
  • Convair Model 58-9: a proposed supersonic transport. Developed by Convair in 1961, it was intended to carry 52 passengers faster than Mach 2.

Operators 2


  • United States: United States Air Force

Convair B-58A Hustler Specifications 2


General Characteristics

  • Crew: 3
  • Length: 96 ft 10 in (29.51 m)
  • Wingspan: 56 ft 9 in (17.30 m)
  • Height: 29 ft 11 in (9.12 m)
  • Wing area: 1,542 sq ft (143.3 m2)
  • Aspect ratio: 2.09
  • Airfoil: root: NACA 0003.46; tip: NACA 0004.08
  • Empty weight: 55,560 lb (25,202 kg)
  • Gross weight: 67,871 lb (30,786 kg)
  • Max takeoff weight: 176,890 lb (80,236 kg)
  • Zero-lift drag coefficient: CD0.0068
  • Frontal area: 10.49 sq ft (0.975 m2)
  • Powerplant: 4 × General Electric J79-GE-5A afterburning turbojet, 10,400 lbf (46 kN) thrust each dry, 15,000 lbf (67 kN) with afterburner

Performance

  • Maximum speed: 1,146 kn (1,319 mph, 2,122 km/h) at 40,000 ft (12,000 m)
  • Maximum speed: Mach 2.0
  • Cruise speed: 530 kn (610 mph, 980 km/h)
  • Range: 4,100 nmi (4,700 mi, 7,600 km)
  • Combat range: 1,740 nmi (2,000 mi, 3,220 km)
  • Service ceiling: 63,400 ft (19,300 m)
  • Rate of climb: 17,400 ft/min (88 m/s) at gross weight
  • Lift-to-drag: 11.3 (subsonic, "clean configuration")
  • Wing loading: 44 lb/sq ft (210 kg/m2)
  • Thrust/weight: 0.919

Armament

  • Guns: 1 × 20 mm T171 cannon
  • Bombs: 1 × Mark 39 or B53 or 4 × B43 or B61 nuclear bombs; maximum weapons load was 19,450 lb (8,820 kg)

Avionics

  • AN/APB-2 Bombing radar
  • AN/APN-110 Doppler navigational radar (part of Sperry AN/ASQ-42 Navigation & Bombing System)
  • AN/APN-170 Terrain-following radar
  • AN/APR-12 Radar warning receiver
  • Hughes Aircraft AN/APQ-69 podded Side looking airborne radar (mounted on RB-58A)
  • Goodyear AN/APS-73 podded synthetic aperture radar (mounted on RB-58A)

References


  1. Shupek, John. The Skytamer Photo Archive, photos by John Shupek, copyright © 2000 Skytamer Images (Skytamer.com)
  2. Wikipedia, the free encyclopedia. Convair B-58 Hustler

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