Boom XB-1
Trijet supersonic demonstrator aircraft From Wikipedia, the free encyclopedia
The Boom XB-1 "Baby Boom" is a one-third-scale trijet supersonic demonstrator designed by Boom Technology (dba "Boom Supersonic"[2]) as part of development of the Boom Overture supersonic transport airliner. Powered by three General Electric J85s, it is planned to maintain Mach 2.2, with over 1,000 nautical miles (1,900 km; 1,200 mi) of range. The XB-1 began taxi tests in December 2022,[3] and conducted its maiden flight on March 22, 2024.[1]
| XB-1 ("Baby Boom") | |
|---|---|
 | |
| Early design of the XB-1 demonstrator | |
| Role | Supersonic technology demonstrator aircraft |
| National origin | United States |
| Manufacturer | Boom Technology |
| First flight | March 22, 2024[1] |
| Status | In flight testing as of March 2024 |
| Number built | 1 |
The design was unveiled in Denver, Colorado, on November 15, 2016,[4] and it was initially intended to make its first subsonic flight in late 2017, powered by three General Electric CJ610 turbojets (a civilian J85), with subsequent supersonic flight testing at Edwards Air Force Base, California.[5]
By April 2017, enough financing was secured to build and fly it.[6] Its preliminary design review was completed by June 2017, with a switch of engine to the military version of the J85 to take advantage of its extra thrust. It was then anticipated that flight tests would start late 2018.[7] In 2017, the composite wing spar was load tested while being heated in a hydraulic testbed at 300 °F (149 °C), above the heat soak operational temperature. First expected supersonic flight slipped to 2019.[8]
By July 2018, the aerodynamic design was completed, the horizontal tail assembled, and the engines received. The Spaceship Co., manufacturer of Virgin Galactic's vehicles, was announced as a partner for flight tests in Mojave, California.[9] Flight tests were delayed again for 2019 due to challenging aerodynamics and further engine change; from the 3,500 pounds-force (16,000 N) J85-21 to the 4,300 lbf (19 kN) J85-15.[9]
The XB-1 design went through three sets of wind tunnel tests. The first indicated that predicted calibration was off by 30%. The second set of tests confirmed accurate calibration, and a third set of tests confirmed design safety. The tunnel testing finished in November 2018, including takeoff and landing with gear doors' impact on stability as well as supersonic inlet testing. These tests had taken a decade on Concorde. The carbon-fiber layup of the fuselage halves was to begin in early 2019 for final assembly of the forward fuselage at the beginning of Spring. With total investment rising to $200 million, Boom was funded for XB-1 flight-testing to the end of 2020.[10] At the June 2019 Paris Air Show, Blake Scholl announced the date for first flight was pushed out to 2020, six months later than previously planned after including a stability augmentation system for better safety at high speed and at take-off and landing.[11]
In February 2020, with the completion of Boom's second simulator, tests began on XB-1 flight controls and system integration.[12] Static wing loading tests were carried out in March 2020, and the wings were mated to the fuselage in April[13] with the aft fuselage nearing completion in May.[14][better source needed] Engines and landing gear were installed later in August and September 2020.[15]
Testing
On October 7, 2020, Boom rolled out the XB-1 in a promotional, with an announcement that the maiden flight was expected in 2021.[16] In early 2021, it was expected to be flight tested around September 2022.[17] On July 26, 2021, Boom began testing and evaluating a forward-looking vision system (FLVS) as part of preparations for flight tests of the XB-1.[18]
In January 2022, Boom began conducting engine run-ups using the XB-1, in preparation for taxi tests and the first flight later in 2022.[19] In May 2022, ground testing was completed with engine run up done on all three engines. Undercarriage and flight systems were tested and deemed ready. Taxi runs and actual flight runs were expected in late 2022.[citation needed] Further delays as of February 2023[update] pushed the expected first flight to mid-2023.[20]
In August 2023, the aircraft received its experimental certification of airworthiness from the FAA.[21] Medium-speed taxi testing was performed in November 2023, with the aircraft reaching a top speed of 94 knots.[22] Following testing, in January 2024 Boom delayed the first test flight to early 2024 to implement safety improvements. The three improvements identified were upgrading the landing gear for increased reliability, optimizing engine intakes for improved resistance to engine stall, and adjusting the aircraft's dampers for improved stability and control.[23]
The XB-1 took its first flight on March 22, 2024, flown by Chief Test Pilot Bill "Doc" Shoemaker from Mojave Air and Space Port.[1]
On April 16, 2024, the FAA issued a special license for the XB-1 to exceed Mach 1 at the nearby Black Mountain Supersonic Corridor. Test flights to Mach 1.1, 1.2 and 1.3 are planned for later in 2024.[24]
The XB-1 Baby Boom is 68 feet (21 m) long with a 17 ft (5.2 m) wingspan and a 13,500-pound (6,100 kg) maximum take-off weight. Powered by three J85-15 engines with variable geometry inlets and exhaust, the prototype should be able to sustain Mach 2.2 with more than 1,000 nmi (1,900 km; 1,200 mi) of range.[4] As a technology demonstrator for the Boom Overture, the XB-1's trijet configuration matched that of the Overture. In 2022, the Overture was redesigned to a quadjet configuration.[citation needed] The XB-1 retains the original trijet configuration.
It has a planned two-crew cockpit, with only one seat being fully developed in the demonstrator, and features a chined fore-body and swept trailing edges.[4] For thermal control, the environmental control system uses the fuel as a heat sink to absorb cabin heat.[8] The space for a second seat is taken up by testing equipment.[25]
Materials
The XB-1 is constructed of lightweight composites, titanium and A286.[25] Materials for the hot leading edges and 307 °F (153 °C) nose, and epoxy materials for cooler parts, are provided by Dutch TenCate Advanced Composites, high-temperature materials supplier for the SpaceX Falcon 9.[8] The airframe will be primarily intermediate-modulus carbon fiber/epoxy, with high-modulus fibers for the wing spar caps and bismaleimide pre-preg for the high-temperature leading edges and ribs.[8] The rear section of fuselage containing the engines is made from 90% titanium and 10% A286 stainless steel alloys.[25]
Data from Aviation Week[4][needs update]
General characteristics
- Crew: 1 (Design allows for a second seat)
- Length: 68 ft (21 m)
- Wingspan: 17 ft (5.2 m)
- Height: 17 ft 0 in (5.2 m)
- Max takeoff weight: 13,500 lb (6,123 kg)
- Powerplant: 3 × General Electric J85-15[9] turbojet, 4,300[9] lbf (19 kN) thrust each
Performance
- Maximum speed: Mach 2.2
- Range: 1,000 nmi (1,200 mi, 1,900 km)
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