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Thrust2

Thrust2 is a jet-propelled vehicle designed and built to challenge and surpass the existing world , achieving an average speed of 633.468 mph (1,019.47 km/h) over a measured mile on October 4, 1983, at the in , . Initiated in 1977 by entrepreneur Richard Noble with an initial budget of just £175 from the sale of his previous project, Thrust1, the vehicle was engineered by designer John Ackroyd and constructed primarily on the Isle of Wight, overcoming significant financial, technical, and logistical challenges including funding shortages, weather delays, and mechanical failures. Powered by a single Rolls-Royce Avon turbojet engine capable of producing approximately 17,000 pounds of thrust, Thrust2 featured a lightweight aluminum chassis with a streamlined body optimized for aerodynamic stability at extreme speeds, targeting a potential top velocity of 650 mph. Driven by himself, a former pilot, the car successfully broke the previous record held by the , ending a 13-year dominance and reclaiming the title for —a feat not accomplished since 1927. Thrust2 maintained the record for nearly 14 years until it was surpassed in 1997 by the supersonic , another Noble-led project that achieved 763 mph with pilot Andy Green. Today, the vehicle is preserved and displayed at the in , , symbolizing a pivotal era in innovation and British engineering perseverance.

Development

Conception

Richard Noble, born in 1946 in , , began his professional career as a paint salesman for before venturing into entrepreneurial pursuits, including leading expeditions such as a journey from to . As a dedicated racing enthusiast from a young age, Noble drew inspiration from historic land speed attempts, particularly John Cobb's fatal 1952 bid with the jet-powered on , which he witnessed as a child, as well as Sir Malcolm Campbell's Blue Bird cars and Craig Breedlove's Spirit of America jet vehicles that dominated records in the . The Thrust2 project was conceived by Noble in 1977–1978, driven by his ambition to restore Britain's prestige in speed records, which had eluded the nation since John Cobb's 1947 world land speed mark of 394.196 mph with the Rail Zeppelin. This initiative stemmed from Noble's frustration with the dominance of American efforts like Breedlove's and his belief that British engineering could reclaim global leadership through innovative design. He founded Project Thrust in 1974 to pursue this vision, emphasizing a fully British-built vehicle to symbolize national ingenuity. Funding the endeavor proved challenging from the outset, with relying heavily on personal investment, including the sale of his to acquire a surplus . Early sponsorship efforts gained traction at the 1977 Motor Show, where public interest led to commitments from companies like TI Group, which donated a spaceframe design after a modest £65 investment in a business lunch, and , which provided initial support among approximately 200 British firms that eventually contributed £1.7 million overall. The project's core objectives centered on surpassing 600 mph via , prioritizing British-sourced components and expertise to achieve a verifiable two-way average under rules, with a smaller test , Thrust1, planned to refine and before full-scale construction.

Thrust1 Prototype

The Thrust1 served as a critical proof-of-concept for validating the principles behind Thrust2, focusing on high-speed , integration, and . Built between 1974 and 1977 in Noble's garage in using a modified , it utilized a rudimentary structure powered by a single Mark 8 sourced from a . The measured approximately 20 feet in length and aimed to demonstrate feasibility for speeds exceeding 650 mph in the final . Testing occurred in 1977 at , where initial runs reached around 150 mph before a bearing caused a crash, destroying the vehicle. This incident provided essential early lessons on structural integrity and component reliability, informing Thrust2's evolution, such as the need for robust design and better systems. Although limited in scope, Thrust1 confirmed the viability of for land speed vehicles while highlighting risks of amateur construction.

Construction of Thrust2

Construction of Thrust2 began in 1978 under the leadership of , who initiated the project to challenge the world after the Thrust1 prototype's failure. The design and primary assembly were handled by engineer John Ackroyd, who worked in rudimentary conditions—a derelict shed in Fishbourne on of —using a limited budget that emphasized practical engineering over advanced facilities. This approach allowed for iterative development, with initial testing in 1980 at yielding six new British speed records at up to 248.87 mph and informing refinements ahead of the full-scale build completion in 1981. Drawing lessons from the Thrust1 prototype's structural failure during high-speed testing in , the team opted for a robust tubular steel frame clad in aluminum panels to balance strength, lightness, and manufacturability. The resulting measured 8.28 meters in length, 2.54 meters in overall width (2.13 meters body width), and 1.37 meters in height to the engine hood (2.13 meters to tail fins), with a total weight of approximately 3,859 kg, enabling the vehicle to achieve the necessary stability and performance for record attempts. Central to the build was the integration of a single 302 jet engine equipped with reheat, sourced from surplus aircraft stock and bench-tested by Rolls-Royce engineers to maximize output at around 17,000 lbf of thrust. The fuel system, based on (Jet A-1), was designed for high-capacity delivery to support sustained high-thrust runs, with additional pumps installed to optimize fuel flow during operation. Ackroyd's hands-on role extended to fabricating key components, ensuring the vehicle's compact, streamlined form while accommodating the engine's central mounting for optimal weight distribution.

Design and Specifications

Chassis and Structure

The chassis of Thrust2 was designed as a fully triangulated to provide high rigidity while supporting all mechanical loads, including the substantial forces from the . Constructed primarily from Reynolds 531 tubing, known for its excellent strength-to-weight ratio, the frame incorporated square and rectangular sections for most elements, with round tubing used selectively in areas requiring bending resistance, such as the roll bars. Two full-length ladder-type longerons formed the core structure, ensuring under high-speed conditions. The body structure integrated seamlessly with the , utilizing internal webs and bulkheads for reinforcement, along with external frames and skin panels to form a semi-monocoque-like without relying on a full . Aluminum sheets—L73 for flat panels and NS4 half-hard for folded or curved sections—were employed for the outer skin, which was flush-finished to minimize aerodynamic drag while allowing removable hatches for . Compound curvatures were avoided where possible, favoring slab surfaces blended into single curvatures to simplify fabrication and enhance structural . The prioritized minimal weight without compromising durability, contributing to the vehicle's overall approximate weight of 3,859 kg. Thrust2 measured 8.28 m in length, 2.54 m in width, and 2.37 m in height (including tail fins), with a of 6.35 m to optimize at extreme speeds. It featured a four-wheel configuration with two front wheels and two rear wheels, the latter mounted externally in the shadow of the Kamm tail for enhanced mechanical and aerodynamic balance. was engineered at 64% over the front wheels and 36% over the rear, positioning the center of gravity approximately 2.29 m behind the front axle to promote lateral and counteract the rear-mounted . clearance was limited to a maximum of 0.100 m, and front wheels measured 0.762 m in , with the front narrower than the rear to accommodate aerodynamic fairings and steering geometry. Wheels were crafted from forged L.77 aluminum alloy, offering a tensile strength of 450 MPa, and were hand-forged, machined, and impact-peened by H.D.A. Limited to withstand the immense stresses of high-speed runs. The space frame approach allowed for iterative testing during development, providing a rigid platform for aerodynamic trials without locking in a final body configuration prematurely. Structural validation included preliminary scale-model wind tunnel tests at British Aerospace facilities to assess overall stability, though specific static load or finite element analyses were not detailed in primary design records.

Propulsion and Powertrain

The propulsion system of Thrust2 centered on a single afterburning 302 turbojet engine, sourced from the fighter aircraft and modified for ground use. This engine delivered a maximum of 17,000 lbf (75.6 kN) with reheat engaged, providing the raw power necessary for extreme acceleration without reliance on mechanical transmission components. The employed direct , where the 's exhaust propelled the rearward, eliminating the need for a gearbox, driveshafts, or as found in wheeled automobiles. The was centrally mounted within the tubular steel chassis for optimal and , with startup achieved via a Palouste compressor providing . control was managed through a cable-operated quadrant adapted from , while ignition relied on standard electrics for reliable simultaneous activation. The consisted of two saddle-shaped tanks, each with a 62-- capacity for a total of 124 (approximately 564 liters) of aviation kerosene (Avtur), positioned near the center of to maintain balance during high-speed runs. These tanks featured rubber bladders filled with Atomel anti-explosive foam to mitigate risks, and was delivered under via a two-stage boost operating at 40 , driven by a high-pressure fueldraulic tapping into the engine's at 1,600 and 5,000 rpm to prevent at supersonic speeds. In full reheat, the engine consumed about 1 per second, enabling a typical 60-second run to use around 60 while providing sufficient margin for the vehicle's operational duration. This configuration allowed Thrust2 to achieve rapid acceleration, reaching speeds exceeding 600 in approximately 20 seconds under optimal conditions, with peak power output sustained beyond 0.8.

Aerodynamics and Safety Features

The design of Thrust2 emphasized minimizing and ensuring at extreme speeds, featuring a long, slender with a Kamm to truncate the efficiently and a curved transition at the nose-wheel arch to reduce effects. The incorporated a 3-degree adjustable for the incidence, allowing optimization of downthrust generated at the front wheels, which was balanced by an upswept rear underbody. Wheel fairings enclosed the front wheels within the envelope to streamline , while a prominent fin provided essential yaw , preventing the from being shrouded by s at high velocities. testing played a crucial role in refining these elements, with preliminary 1/10-scale models evaluated at in Bristol for overall shape, moving-ground simulations at the to assess ground-effect interactions, and tests at using 1/30-scale models up to 0.86 to minimize formation and rise beyond 300 . These efforts resulted in a predicted of approximately 12,000 pounds at the target speed of 650 , enabling the to achieve its record-breaking performance. Safety features were integrated to protect driver during high-speed runs and deceleration, including a reinforced with ergonomic arm rests and a system that allowed the driver to hang securely in straps during maneuvers. A dual parachute deployment system provided braking and stabilization: a high-speed setup with a single 7.5-foot-diameter chute on a 100-foot towline for use above 375 , and a low-speed configuration deploying three 7.5-foot chutes on 50-foot towlines, each system capable of generating up to 22,000 pounds of for nearly deceleration. Fire suppression was addressed through accessible extinguishers operable by the driver's right hand from the controls, which also included buttons on the for chute release. These measures, combined with the vehicle's straight-line focus and precise steering, were critical for handling supersonic conditions without compromising structural integrity. The tires and wheels were engineered for durability under bursts exceeding 600 , utilizing custom aluminum discs with a 30-inch —forged from L.77 rated at 450 (29 tons per ) for strength. Front wheels measured 6 inches wide to support 64% of the vehicle's , while rear wheels featured a keeled design to promote understeer stability; the unsprung was kept to 9% of the total to minimize dynamic loads. These wheels, rotating up to 8,000 rpm (equivalent to 705 ), eliminated the risks associated with pneumatic tires at such velocities, ensuring reliable contact with the surface during record attempts.

Record Attempt

Preparation and Team

The Thrust2 project, initiated by in 1977, culminated in extensive preparations for the 1983 world attempt, focusing on logistical, technical, and operational readiness after years of development on a shoestring budget. The location selected was the in , , prized for its vast, flat salt surface exceeding 12 miles in length, which provided the necessary straight-line distance for high-speed runs and received approval from the (FIA) for official record attempts. This choice followed unsuccessful efforts at the due to adverse weather, marking Black Rock as the ideal venue for the team's return in 1983. The core team was led by , who served as both project director and driver, alongside chief designer and engineer John Ackroyd, whose expertise shaped the vehicle's innovative structure. Supporting them was a dedicated of engineers, mechanics, and technicians, including early members like Ron Benton and others such as Terry Hopkins, Geoff Smee, Tony Meston, Ed Elsom, and Gordy Flux, who contributed to fabrication and testing phases. The full support team for the 1983 attempt numbered in the dozens, handling everything from vehicle maintenance to data analysis under resource constraints. Pre-run testing emphasized shakedown runs to validate the vehicle's stability and performance, beginning with low-speed trials in the at in 1980, where Thrust2 achieved a record of 248 without its full bodywork. Further testing occurred , including attempts at Bonneville in 1981 and initial runs at in 1982, allowing the team to refine handling and engine response incrementally. Instrumentation preparation involved installing timing systems, basic for real-time data on speed and engine parameters (using pre-GPS radio-based tracking), and safety monitoring equipment to ensure precise measurements compliant with FIA standards. Weather monitoring was critical, with the team tracking conditions to avoid rain-slicked surfaces that had previously halted efforts, prioritizing dry, hot periods for optimal . Logistics for the 1983 campaign were meticulously planned despite financial limitations, with the Thrust2 vehicle and equipment transported across to the via sea freight and overland haulage. The team established a base camp at by late August 1983, setting up workshops, fuel storage, and living quarters in the remote to support the intensive two-month operation leading to the record runs. This setup enabled rapid adjustments between test sessions, underscoring the project's reliance on efficient, low-cost operations.

The 1983 Runs

The Thrust2 team's record attempt culminated on October 4, 1983, at the in , following several days of practice runs to familiarize driver with the vehicle's handling at extreme speeds. Earlier runs in the preceding weeks and mornings had progressively built confidence, with Noble completing multiple passes exceeding 600 to refine steering inputs and stability techniques, such as subtle corrections using the armrests to counter high-g lateral forces. The bed surface, marked with painted lines to define the 13-mile course, provided a stable, virtually stone-free track essential for the high-speed traverses. The official attempts adhered to Fédération Internationale de l'Automobile (FIA) protocols, requiring a two-way speed over measured one-mile timing traps, with the return run completed within one hour of the forward pass to qualify for the record. On that day, conditions were optimal with dry and winds within acceptable limits for ratification, allowing the team—led by er John Ackroyd and a small support crew—to prepare the vehicle efficiently between runs by refueling, repacking parachutes, and inspecting the course. Noble's forward run clocked 624 mph through the mile trap, affected by a slightly draggy setup and initial hesitation from a blown fuse, yet demonstrating the car's potential under full thrust. For the return run, the maximized the run-up distance and adjusted for hotter temperatures, which raised the and aided . achieved 643 over the mile, peaking at 650.88 before deploying the parachute , which induced a 6g deceleration at 120 per second to halt the vehicle safely. During these passes, reported intense vibrations above 500 giving way to a smoother ride beyond 600 , where he could relax and observe supersonic shock waves forming on the engine housing and wheel arches, maintaining through precise and with left foot on the and right on the . The two runs yielded an official two-way average of 633.468 (1,019.47 km/h), surpassing the previous .

Challenges Encountered

During the preparation and execution of the 1983 record attempt at , the Thrust2 team grappled with significant mechanical challenges. Early tests revealed issues with the , including a dangerous surge that nearly destroyed the unit, necessitating precise recalibrations to the fuel pumps and reheat system to ensure stable operation. Additionally, at speeds approaching 400 mph, the vehicle experienced pronounced shimmy, which compromised ; this was addressed through iterative refinements to the solid design, including wider 6-inch front wheels and optimized tread patterns in the configuration. Environmental conditions at the remote Black Rock playa presented further obstacles, with dust storms and heavy rains delaying runs for weeks and complicating track preparation. The surface proved softer than anticipated, cracking under the intense heat generated by the tires during high-speed passes and forming deeper ruts that rendered track reuse impractical, forcing the team to "consume" fresh sections of the playa for each run. Human factors also demanded careful management, particularly driver fatigue for , whose training regimen was restricted to brief sessions totaling just 12 minutes of cumulative driving time to hone technique while minimizing exhaustion risks during the intense, short-duration attempts. Communication with timing crews occasionally faltered due to the isolated desert setting and rudimentary radio setups, but these were mitigated through redundant signaling protocols. To overcome these hurdles, the team relied on on-site repairs, such as and adjustments, alongside backup systems like dual drag chutes with separate high- and low-speed deployments and redundant electrical circuits for reliability. Iterative tweaks, informed by detailed data logs from prior tests, allowed for rapid adaptations, while the vehicle's inherent aerodynamic above 240 provided a foundational for handling issues.

Achievements

Breaking the Record

On October 4, 1983, at the in , piloted Thrust2 to a historic breakthrough, surpassing the previous of 622.407 mph set by in the rocket car on October 23, 1970. Thrust2 achieved a two-way average speed of 633.468 mph over the measured mile, with a peak speed of 650.88 mph, marking a significant advancement in jet-propelled land speed technology. Noble later recounted the run's sensations as remarkably composed despite the extreme velocity. Accelerating at 2G from the start, he described the car above 600 as "pure magic," allowing him to discern every detail while observing supersonic shock waves forming on the housing and arches. Deceleration via the parachute brake was intense, shedding speed at 120 per second, though Noble found the drop back to 400 "boring" enough to jokingly consider walking. Immediately after, the team's radio crackled with confirmation: "That’s 642.971 for the mile and together that’s a new record of 633.468 . Congratulations," sparking jubilation among the crew as the flag waved in celebration of reclaiming the outright title. The achievement drew immediate global media spotlight, with outlets like reporting the "snap" of the 13-year-old American record by a British jet car, underscoring the national triumph after the title had eluded Britain since Donald Campbell's 403.10 mph mark in 1964. Press reactions celebrated Noble's feat as a resurgence of British engineering prowess, highlighting how Thrust2's success restored national pride in high-speed innovation on the world stage.

Record Details and Validation

The Thrust2 achieved its world through two timed runs over a 1 km flying start distance, with the forward run clocked at 1,017.46 km/h and the return run at 1,021.35 km/h, yielding an average speed of 1,019.4 km/h (633.468 mph). These trap speeds were precisely measured using FIA-approved photo-timers positioned at the start and end of the measured kilometer to capture the vehicle's passage with high accuracy. Validation of the record was conducted by (FIA) officials, who performed comprehensive inspections of the Thrust2 vehicle, the course layout, and all collected data to confirm adherence to FIA regulations outlined in Appendix D of the . The process emphasized the requirement for two opposing-direction runs completed within a one-hour window, ensuring the average speed accounted for varying wind and surface conditions while minimizing environmental influences. Supporting instrumentation included optical sensors integrated with the photo-timers for timing the runs and barographs to altitude variations and wind profiles along the course, all calibrated to maintain error margins below 0.1% for reliability. This setup allowed for verifiable , with post-run analysis confirming no discrepancies in vehicle performance or measurement protocols. The achievement represented a 1.78% improvement over the prior .

Legacy

Post-Record Use and Preservation

Following the successful record-breaking runs in the Black Rock Desert on October 4, 1983, Thrust2 was returned to the , where it embarked on a series of promotional tours across the country to celebrate the achievement and raise awareness of British engineering prowess. These tours included appearances at various motorsport events and public exhibitions, allowing thousands to view the vehicle up close in the years immediately after the record. No additional high-speed runs were attempted, as the focus shifted to preservation and public display. In 1986, the Thrust team placed Thrust2 on permanent loan to the , recognizing the institution's strong ties to the British automotive industry. The car quickly became a centerpiece of the museum's collections, featuring in a dedicated multi-media titled "The Fastest Car on Earth" launched in 1987, which included a 12-projector audio-visual presentation and documentary footage of the record attempt. It was occasionally loaned out for special events and motorshows during this period, but remained primarily static. In March 1993, following a public fundraising campaign, the museum acquired full ownership of Thrust2 from the original Thrust team, ensuring its long-term security. Preservation efforts have centered on maintaining the vehicle's structural integrity and historical authenticity, given its static display status. During the museum's major redevelopment in 2014, Thrust2 was carefully relocated using cranes and specialized equipment to its new home in the Land Speed Gallery, alongside and , as part of an £8.5 million upgrade that enhanced visitor access and environmental controls. Periodic inspections, including checks on the engine and chassis components, have been conducted in the intervening years to prevent deterioration, though no major restorations have been publicly documented. As of 2025, Thrust2 remains in static exhibition at the , drawing significant visitor interest during anniversary events and serving as a key artifact in the gallery's focus on land speed history. No further operational runs have been planned or executed, aligning with its role as a preserved icon.

Influence on Land Speed Racing

Thrust2's successful use of a single jet engine to achieve a of 633.468 mph in 1983 demonstrated the feasibility of for ultra-high-speed vehicles, paving the way for more advanced configurations in subsequent record attempts. This technological validation influenced the design of , which employed dual engines to reach 763.035 mph in 1997, marking the first supersonic . By pushing the limits of subsonic engineering, Thrust2 established key principles in thrust management and aerodynamic stability that informed the evolution of propulsion systems in . The vehicle's achievement revived British interest in , returning the outright world record to the for the first time since and inspiring a of engineers and enthusiasts. This resurgence directly led to project leader Richard Noble's initiation of the program, which built on Thrust2's legacy to target supersonic speeds. Andy Green, who later piloted to its record, became involved through this chain of British-led efforts, highlighting how Thrust2 fostered talent and collaboration in the field. Thrust2 also elevated safety standards in through its innovative braking systems, including ribbon deployed sequentially to decelerate from over 600 mph, which became a for high-speed stopping mechanisms. These advancements contributed to refinements in for even faster , emphasizing and load management. Furthermore, the project's success prompted evolutions in FIA regulations, particularly for thrust-powered cars, incorporating requirements for aerodynamic analysis in and supersonic regimes to accommodate attempts beyond Mach 1. As of 2025, Thrust2 remains a symbol of 1980s engineering ingenuity, frequently referenced in the revival of the project as one of the few vehicles to exceed 600 mph and a foundational milestone in the pursuit of new records. Thrust2 held the outright until 1997, when it was surpassed by .

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