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Aircraft And Military Development & Applications
9-Bell X-2 Starbuster
The Bell X-2 nicknamed "Starbuster" was an X-plane research aircraft built to investigate flight characteristics in the Mach 2-3 range. The X-2 was a rocket-powered, swept-wing research aircraft developed jointly in 1945 by Bell Aircraft Corporation, the U.S. Air Force and the National Advisory Committee for Aeronautics to explore aerodynamic problems of supersonic flight and to expand the speed and altitude regimes obtained with the earlier X-1 series of research aircraft.
Maximum speed: 3,370 km/h (2,094 mph) Maiden flight: 18 Nov 1955 Length: 37.83 ft Wingspan: 32.15 ft Passengers: 1 Retired: 27 Sep 1956
The Bell X-2 was a rocket-powered, swept-wing research aircraft designed to investigate the structural effects of aerodynamic heating as well as stability and control effectiveness at high speeds and altitudes. The program was developed jointly in 1945 by Bell Aircraft Corporation, the U.S. Air Force and the National Advisory Committee for Aeronautics (NACA) to explore aerodynamic problems of supersonic flight and to expand the speed and altitude regimes obtained with the earlier X-1 series of research aircraft.
In 1946, the NACA Pilotless Aircraft Research Division (PARD) began testing rocket launched X-2 models at Wallops Island, VA, to gather stability and c ontrol data. Additional tests helped NACA and Bell engineers
design a pilot escape system for the X-2. The NACA made its spin tunnel and supersonic wind-tunnels at the Langley Memorial Aeronautical Laboratory, Hampton, VA, available to evaluate various aspects of the X-2 design. The NACA was also responsible for scientific instrumentation of the X-2.
Two X-2 airframes, nicknamed "Starbuster," were built at Bell's plant in Wheatfield, NY, using stainless steel and K-monel (a copper-nickel alloy). The vehicles were designed to employ a two-chamber Curtiss-Wright XLR25 throttleable liquid-fueled rocket engine. It had a variable thrust rating from 2,500 to 15,000 pounds. The X-2 was equipped with an escape capsule for the pilot. In an emergency, the entire nose assembly would jettison and deploy a stabilizing parachute. Once at a safe altitude, the pilot would then manually open the canopy and bail out. Although the Air Force approved the final escape system design, NACA representatives were concerned that it might prove dangerous to use.
A Boeing B-50A bomber was modified to carry the X-2 to launch altitudes around 30,000 feet. The pilot then climbed into the X-2, dropped away from the bomber, and ignited the engines if it was a planned powered flight. After engine burnout, the pilot guided the X-2 to an unpowered landing on the surface of Rogers Dry Lake at Edwards Air Force Base, CA.
The X-2 (46-674) drops away from its Boeing B-50 mothership. Lt. Col. Frank "Pete" Everest piloted 674 on its first unpowered flight on 5 August 1954.
Because of a decision to install the first available engine in airframe 46-674, airframe 46-675 was delivered to Edwards first for glide tests. It arrived at Edwards on April 22, 1952. After two captive flights, Bell test pilot Jean L. "Skip" Ziegler made the first glide flight on June 27. A rough landing caused some damage to the aircraft and the second glide flight was delayed until Oct. 8. Two days later, Air Force test pilot Maj. Frank K. "Pete" Everest successfully completed the third glide flight of the X-2.
Following the unpowered tests, the X-2 was returned to Bell's plant in New York. The engine had not yet been installed in the first X-2, 46-674, so it was installed in the second shortly after it returned to Wheatfield. Captive flights with the new engine were carried out over Lake Ontario. During a flight to check the liquid oxygen system, an explosion resulted in the loss of the X-2 and severe damage to the B-50. Skip Ziegler and B-50 crew member Frank Wolko were both killed. The X-2 fell into Lake Ontario and was not recovered. The B-50A was damaged beyond economic repair and was subsequently replaced with a modified B-50D.
The following day, it began its journey to Edwards beneath the B-50D. The aircraft arrived on July 15 and technicians at the NACA High Speed Flight Station (HSFS) began to install instrumentation to gather handling qualities data. On the advice on the NACA, the Air Force purchased a Goodyear Electronic Digital Analyzer (GEDA) analog computer. Richard E. Day, NACA project engineer for the X-2, programmed the GEDA and turned it into a rudimentary flight simulator for the aircraft.
On Aug. 5, 1954, the X-2 was carried aloft for another captive flight beneath the B-50. Later that day, the X-2 was carried aloft for a second time and released. Pete Everest, now a lieutenant colonel, made a successful glide flight that ended in a rough landing on the lakebed. The vehicle sustained minor damage and was returned to Wheatfield for repair.
The X-2 returned to Edwards on Jan. 16, 1955, and captive flights resumed on Feb. 5 for propellant system checks. After several captive missions, two more glide flights were accomplished in March and April. Damage to the aircraft during landing required the X-2 to return to New York once again.
The first attempt at a powered flight took place on Oct. 25, 1955, but a nitrogen leak resulted in a decision to change the flight plan. Everest completed the mission as a glide flight. An aborted second attempt ended as a captive flight. Everest finally made the first powered X-2 flight on Nov. 18, igniting only the 5,000-pound-thrust chamber. His maximum speed during the mission was Mach 0.95. Following several aborted attempts, Everest completed a second powered flight on March 24, 1956, this time only igniting the 10,000-pound-thrust rocket chamber.
Both chambers were used for the first supersonic X-2 flight on April 25. The airplane reached a speed of Mach 1.40 and a maximum altitude of 50,000 feet. Everest completed three flights in May that pushed the airplane's speed envelope to Mach 2.53. On May 25, 1956, a new pilot was checked out in the X-2, Capt. Iven C. Kincheloe. He made a successful supersonic flight, but had to shut the engine down prematurely due to a malfunction. In June, the airplane was grounded for installation of engine nozzle extensions to improve performance. Everest made a supersonic checkout of the modified X-2 on July 12. Everest's final X-2 flight, on July 23, 1956, earned him the title "Fastest Man Alive." While gathering data on aerodynamic heating, Everest achieved a speed of Mach 2.87 at 68,000 feet.
Kincheloe now assumed the role of X-2 project pilot for a series of high-altitude missions. After two aborted flight attempts, he successfully accomplished a climb to 87,750 feet while gathering stability data on Aug. 3, 1956. That same day, NACA director Hugh L. Dryden requested that the Air Force loan the X-2 to the NACA for research purposes. The Air Force continued to fly the airplane while attempting to achieve its maximum altitude capability. While a flight on Aug. 8, failed to exceed 70,000 feet, another attempt on Sept. 7 reached an altitude of 126,200 feet. This earned Kincheloe the title "First of the Spacemen" and a record that stood until the advent of the X-15 program. Kincheloe made three additional flight attempts, but each ended in an abort.
The Air Force was due to transfer the X-2 to the NACA in mid-September and preparations were underway. Researchers at the NACA High Speed Flight Station were anxious to use the X-2 for heating investigations in the Mach 2 to Mach 3 range and study handling characteristics at extreme altitudes and speeds. The Air Force, however, asked for an extension of their program so that another pilot could be checked out. As Capt. Milburn G. "Mel" Apt practiced simulated missions on the GEDA, representatives from the Air Force, the NACA, and Bell agreed on a flight plan.
On Sept. 27, 1956, Apt became the first person to fly faster than three times the speed of sound. The engine burned slightly longer than expected and Apt flew a near perfect flight profile, allowing him to reach a speed of 2,094 mph (Mach 3.196). Elation was short lived. For some reason, Apt initiated a sharp turn back toward Edwards. This resulted in a control divergence known as inertial coupling. The X-2 began to tumble uncontrollably. Apt jettisoned the escape capsule, but was unable to extract himself before it struck the ground. Apt's death cast a shadow over the most spectacular achievement of the program.
Last Updated: Aug. 4, 2017 NASA Editor: Yvonne Gibbs
Bell X-2 "Starbuster"
The Bell X-2 was a rocket-powered research plane jointly developed by Bell Aircraft Corporation, the U.S. Air Force and the National Advisory Committee for Aeronautics (the precursor to NASA) in 1945. The aircraft was built to investigate aerodynamic issues with supersonic flight within the Mach 2 to Mach 3 range.
The X-2, nicknamed "Starbuster," completed its first powered flight in November 1955. The following year, in September 1956, Captain Milburn Apt was at the controls when the X-2 reached Mach 3.2 (2,094 mph, or 3,370 km/h), at an altitude of 65,000 feet (19,800 m).
Shortly after attaining this top speed, however, Apt tried to turn the aircraft while it was still above Mach 3. The plane tumbled out of control, and Apt's attempts to recover from the spin failed. This tragic accident ended the X-2 program, after a total of 20 test flights.
The Starbuster was an American research aircraft which had its first flight in 1955 and was retired in 1956. It was a continuation of the X-2 program and so Its area of investigation was to see how aircrafts behaved when flying at speeds higher than mach 2.0. It did, as can be understood, not carry any weapons and featured a back-swept wing which made it have little air-resistance and was by that able to achieve the stunning speed of 3.196 mach in 1956. However soon after this speed was attained the pilot, Milburn G. Apt, made a sharp turn and the aircraft tumbled out of control. He could not regain control of the aircraft and bailed out. Unfortunately, only the small parachute of the escape shuttle was opened and he hit the ground with too high speed. This fatal crash ended the Starbuster programme.
Crew: one, pilot
Length: 37 ft 10 in (11.5 m)
Wingspan: 32 ft 3 in (9.8 m)
Height: 11 ft 10 in (3.6 m)
Wing area: 260 ft² (24.2 m²)
Airfoil: 2S-50 bicon
Empty weight: 12,375 lb (5,600 kg)
Loaded weight: 24,910 lb (11,300 kg)
Max. takeoff weight: 24,910 lb (11,300 kg)
Powerplant: 1 × Curtiss-Wright XLR25 rocket engine, 15,000 lbf (67 kN)at sea level
Role: Research aircraft
National origin: United States
Manufacturer: Bell Aircraft
First flight: 18 November 1955 (first powered flight) 27
June 1952 (first drop glide)
Retired: 27 September 1956
Primary users: United States Air Force
National Advisory Committee for Aeronautics
Number built: 2
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