The Supercar Schematics and an initial partially completed cutaway was created by Shane Pickering in 1999 with an update in 2021. The schematics were published in Fanderson’s FAB 98 (July 2021). See
I have tried various AI image generation tools in the last 2 years to see if a reasonably complete Supercar Cutaway could be created, but all gave very poor results. However, the AI tools are improving quickly. So I gave the detailed version of these schematics (PDF link above) to Google Gemini along with Shane’s outline cutaway image as a template.
The result (shown to right, click for larger version) was better than previous attempts which did not even keep the overall vehicle shape. The EMH powerplant and two engines in the rear compartment were confused and do not leave room for the wing retraction sleeve. The whole flow of vertical, horizontal and retro thrust, as well as flows of water and air are not present. The large fuel tanks needed are not accommodated. Ailerons were incorrectly added to the wings. The Clear-Vu would be a 1960s CRT tube, not a flat panel display. Various control panels were wrongly added to one side of the cockpit interior. The large cylindrical object in the nose where the batteries and initial engine charging and backup power mechanism is placed was not what was expected.
I did a bit of manual editing to bring things more closely into line with the 1999 technical schematics, but left in the AI suggested front mounted batteries and charging mechanism, resulting in this image. Note: Shane defintely does not endorse the AI experiment and mangling of his fine technical details.

Supercar Control Plans
Supercar operates in any of a set of “Control Plans” (see section in Schematics PDF) which set up the various systems such as hydraulics, valves, wastegates, instruments, sensors and control computers to respond in appropriate ways to the environment and the pilot’s (or remote console’s) control inputs. The Google Gemini generated illustration below tries to visualise the operation. It includes references to the use of ailerons and elevators in flight which Supercar does not have. Supercar uses vector thrust. Interesting attempt anyway.

Google Gemini generated illustration of the operation of Supercar’s Control Levers
Google Gemini Prompts and Thinking – Supercar Cutaway
Prompt: Create a technical cutaway schematic of “Supercar” using all the details of internal mechanisms and equipment shown in the PDF file at http://www.aiai.ed.ac.uk/~bat/GA/CUTAWAYS/SC/Supercar-Schematics-Details.pdf
Based on the detailed technical schematics and text provided in the document, here is a comprehensive technical breakdown of the Supercar text and drawings by Shane Pickering and Austin Tate.
TECHNICAL CUTAWAY: SUPERCAR PROTOTYPE
1. Propulsion & Powerplant Systems
The vehicle utilizes a dual-engine configuration managed by a central interlock system, allowing for operation in atmosphere, underwater, and space.
Primary Powerplant (EMH): The heart of the vehicle is the EMH® (Electro-Magneto-Hydrodynamic) Powerplant located centrally between the rear engines.
Specs: A superconducting generator with a 0.5-megawatt capacity.
Function: It acts as the primary electrical generator, a self-contained marine motor for water operations, and a booster for the Ramjets during space flight by scooping hydrogen.
Exhaust: Completely clean, emitting only water vapor.
Main Engines (Ramjets): Twin Hybrid, Vectored Thrust, Stratified Turbine Ramjets.
Thrust: Each engine develops in excess of 19,000 lbs of static thrust.
Features: Equipped with afterburners (Turbo Boost), ceramic vectored exhaust nozzles, and oil injectors for smoke screens.
Interlock® Mechanism: A transverse driveshaft and gearbox system that interconnects both engines to ensure safety; if one engine fails, the vehicle remains operational.
Fuel Supply: AvGas: Main tanks contain classified AvGas® for the Ramjets.
Hydrogen/Oxygen: Separate refrigerated liquid Hydrogen and Oxygen tanks are stored forward of the main tank for the EMH unit during space or marine flight.
Intakes: Ram intake valvegates (for air or water) regulate feed and can be closed for ballast operations.
2. Flight & Marine Control Systems
Supercar is a VTOL (Vertical Take-Off and Landing) vehicle capable of “Ground Effect” hovering and submarine operation.
Vectored Thrust:
Rear Nozzles: Ceramic exhaust nozzles divert thrust for forward motion.
VTOL Jets: Four large VTOL jet nozzles are located under the fuselage, featuring CAD (Cushion Augmentation Devices) for stability and “Ground Effect” hovering.
Retro Jets: Twin retro jets on the port and starboard sides provide braking power and sideways maneuvering via heat extractor vanes.
Marine Conversion:
Intake Valves: Hydraulic valvegates close off air intakes before submersion, redirecting water flow directly to the EMH powerplant.
Ballast: Rear and Forward Ballast Tanks can be flooded or blown with compressed air to control buoyancy.
Wings: Retractable wings housed in a “Wing Box Surround” extend for high-speed horizontal flight and retract for parking or confined spaces.
3. Avionics & Sensors
The “brain” of Supercar is housed in the pressurized nose and wing nacelles.
ClearVu® System: Instrumentation: The cockpit features Multi-mode ClearVu® CRT instrumentation for flight data and system status.
Periscope: A retractable receptor on the Hi-Band antenna feeds visual data to the pilot.
Sensor Probes:
Wing Nemacelles: House avionics, marine sensor probes, and INS (Inertial Navigation System) aerials.
Nose Array: Contains the main Radar/Sonar sensor array and “Remote®” pickup receiver.
Remote Control: A “Remote®” receiver allows the vehicle to be piloted or tracked directly from the Black Rock Laboratory console.
4. Life Support & Safety Mechanisms
Designed for extreme environments (depths of 400ft+ and altitudes of 108,000ft+).
Cabin: Pressurized “all-glass cockpit” made of bullet-proof, 1-inch thick, double-glazed acrylic. The Flexiglass® Canopy splits into two halves and slides down internal tracks for entry.
Atmosphere: Oxygen: Regenerators and pressurization pumps recycle air, fed by oxygen bottles embedded in the front seats.
Emergency Recovery: Ballistic Parachutes: Three recovery packs are fitted—one in the nose and two in the rear wing nacelles—to save the “Whole Vehicle” in case of failure.
Emergency Generator: A retractable wind/water-driven turbine in the nose provides backup power if main systems fail, provided the craft has forward motion.
5. Equipment & Storage
Nose Compartment: A forward-mounted “Multi-Purpose Optional Equipment Bay” can house mission-specific gear, such as a Removable Rocket Gun Mount.
Luggage Bay: Located behind the rear folding seats; also houses the auxiliary fuel tank.
Landing Gear: In addition to standard landing capability, the fuselage floor houses twin landing skids that convert into “inverted equipment racks” for magnetic hoists or bomb racks.
Summary of Dimensions & Design
Designers: Originally designed by Reg Hill; technical concepts by Shane Pickering and Austin Tate.
Hull: Insulated alloy hull capable of carrying an electrostatic charge to ward off predators.
Steering: Fly-By-Wire (FBW) computer system simplifies pilot input, coordinating pitch, yaw, and roll.
Would you like me to generate a specific detailed description for one of these sub-systems, such as the Control Plans used to switch between these modes?
Google Gemini Prompts and Thinking – Supercar Control Plans
Prompt: Generate a specific detailed description for the Control Plans used to switch between these modes?
Based on the retro-futuristic design of the craft (reminiscent of the Supercar or similar Gerry Anderson-style vehicles), here is a detailed technical description of the Control Systems and Operational Sequences (Control Plans) used to switch between its primary operating modes: Aero (Flight), Hydro (Marine/Submersible), and VTO/Hover (Ground).
Master Control Console: Mode Switching Architecture
The vehicle utilizes a Tri-State Sequential Actuation System located on the center console between the pilot and co-pilot. Mode switching is not instantaneous; it requires a specific “Control Plan” or sequence of operations to ensure structural integrity during the transition.
1. The Master Mode Selector (MMS)
Physical Interface: A heavy-duty, locking hydraulic lever located on the central pedestal. It moves through a gated shift plate with three distinct detents:
Position 0 (Forward): Aero-High (Atmospheric Flight)
Position 1 (Center): VTO/Hover (Low altitude/Ground effect)
Position 2 (Aft): Hydro-Sub (Marine and Underwater)
Safety Interlock: The lever is guarded by a “Dead Man” solenoid collar. The pilot must lift the collar to disengage the mechanical lock before shifting modes, preventing accidental engagement during high-G maneuvers.
Detailed Transition Sequences (The Control Plans)
Plan A: VTO to Aero (Hover to Flight Transition)
Actuation: Pilot shifts MMS from Center to Forward.
System Response:
“Clear-Vu” Retraction: The vertical lift fans (or repulsor vents) located in the fuselage belly reduce power to 30%.
Wing Deployment: Hydraulic rams extend the variable-geometry wings outward from the fuselage recesses. The wings lock into the “High-Speed Dihedral” position.
Thrust Vectoring: The rear jet exhaust baffles rotate from a 45° downward angle to a 0° horizontal vector.
Intake Expansion: The prominent nose intake louvers (painted yellow/red) open fully to maximize airflow for the main turbine.
Cockpit Indicators: A “WINGS LOCKED” green tell-tale light illuminates on the primary dashboard.
Plan B: Aero to Hydro (Flight to Submersible Transition)
Actuation: Pilot shifts MMS from Forward to Aft (bypassing Center via a rapid-shift override if performing an emergency dive).
System Response:
Atmospheric Sealing: A pneumatic seal inflates around the canopy rim. The main turbine air intakes (nose and side) snap shut, and the system switches to the Closed-Cycle Hydro-Jet propulsion.
Wing Configuration: The wings do not fully retract but pivot 15° downwards to act as hydro-stabilizers (diving planes).
Retraction: The vertical stabilizer (tail fin) telescopes downward slightly to reduce drag profile in water.
Periscope/Sensor Array: The dorsal antenna array retracts, and the sonar dome (located on the chin of the craft) activates.
Cockpit Indicators: The altimeter automatically swaps inputs to become a Depth Gauge. Cabin pressure is equalized to 1 ATM.
Plan C: Operations & Handling (The Control Surfaces)
Once a mode is selected, the Yoke/Steering Controls adapt their sensitivity:
In Aero Mode: The yoke controls ailerons and elevators via standard fly-by-wire.
In VTO Mode: The yoke translates to lateral thrusters for strafing/turning on a dime.
In Hydro Mode: The rudder pedals become sensitive for water-jet steering, and the yoke controls pitch (diving/surfacing) via the hydrofoils.
Emergency Override: The “Crash Dive” Protocol
A specific red toggle switch labeled “EMERGENCY BALLAST” is located above the main screen. Flipping this:
Instantly cuts all main turbine power.
Floods the rapid-descent ballast tanks located in the side pontoons (yellow tubes).
Forces the craft to drop from the sky directly into the water, bypassing the standard sealing delay—used only for immediate evasion.
Defining the Scope
I’m currently focused on defining the precise scope of this visualization. Translating the textual mode-switching descriptions into a clear schematic is key. I’m prioritizing clarity and technical accuracy in this retro-futuristic context.
Refining the Schematic
I’m now diving into the detailed elements of Plan A and B. I need to figure out how to represent the “Dead Man” safety collar integration into the flow. The key focus is on visually clear transitions, from wing deployment to atmospheric sealing. I’m focusing on the interaction between user controls and system feedback in each mode.
Developing the Flowchart
I’m structuring the technical schematic now. The focus is on visually clear transitions, from wing deployment to atmospheric sealing. I’ve begun integrating the “Dead Man” safety collar into the control flow and defining how the “Yoke/Steering Controls” adapt across each mode.
Designing the Visual Schematic
I’m translating the text into a visual, now. The focus is on the schematic’s style, going for a blueprint look with aged aesthetic. Clear icons will represent components, and annotations will be derived directly from the source text to ensure the system responses are represented. I’m prioritizing clarity.
Analyzing Image Details
I’m currently cross-referencing the image’s elements with the user’s initial specifications. I’m focusing on ensuring all the requested components, especially the core ‘Master Mode Selector’ and the designated ‘Transition Sequences’, are present and accurately represented. My aim is to ensure fidelity to the technical instructions.
Reviewing Technical Accuracy
I’m now carefully checking the depiction of the ‘Dead Man’ collar and ‘Emergency Ballast’ protocol. This image impressively aligns with all the technical details outlined, including Plans A, B, and C within the ‘Transition Sequences’. I’m focused on confirming the schematic’s retro-futuristic style resonates appropriately with the user’s initial guidance. The elements are rendered coherently, but need close inspection.
Prompt: For the controls plan image please replace the Master Mode Selector with the four level control selector shown in this image and adjust the control plans to fit in with those four levers
Initiating Schematic Edit
I’m now integrating the four-lever control system into the original schematic. My focus is on achieving a seamless transition, making the new system look like a natural evolution of the existing design. After the integration, I’ll redraw the control plans, ensuring they clearly and logically link to the updated lever arrangement, maintaining the style of a genuine technical drawing.
Updating Lever Integration
I’ve begun the process of integrating the new four-lever system into the original schematic. Currently, I’m focusing on precisely replacing the single lever with the four-lever configuration within the console area. I’m carefully redrawing the connection lines to ensure they logically connect the levers to the existing transition sequences, maintaining a consistent technical drawing style.
Evaluating Complex Interactions
I’ve closely examined the image’s implementation of the control system. The shift to a four-lever setup necessitated a complete rethinking of the internal plans, and those adjustments seem successful. The relationship between the new levers and the overarching system logic is sound.
Reassessing System Logic
My focus is on comparing the image with the initial specifications. The transition to the multi-lever system required a thorough review and re-routing of the master control plans. I’ve confirmed that the logic now correctly integrates with the selector. I’m satisfied that the visual execution reflects the intended function.
Supercar was created by A.P. Film Studios in association with ITC (now ITC Studios). Supercar internal schematic technical concept, text and drawings by Shane Pickering 1999 with assistance from Austin Tate. Original Supercar designed by Reg Hill of A.P. Films. Supercar exterior based on Phil Rae Blueprints and 3-D model by Mick Imrie and Austin Tate. This is fan produced material to promote the shows of Gerry Anderson and provided for your enjoyment, and should not be used for any commercial purpose.