C/M Fast Mach 2 Passenger + Cargo
C/M Fast Passenger + Cargo Supersonic
CYPRESS MOTOR PLANE
C/M may offer a Niche Fast Airline then subsidize alternate Alliance partners
"Break even in 1 year of flight or less"
Cypress Airlines! Vintage Modern
https://2026featurecig.blogspot.com/2026/08/blog-post_968.html
MACH 2 FLIGHT
200 X 9.7 feet in size & 90 Seats unlike Airbus A350 300-480 seats
5 or 6 C/M Mach 2 = equivlance at max of $270 Million Alberta dollars
Zero Emissions. Zero Cycle. Emissions controls
Perpetual Kinetic Energy Generators direct to gained EV Electric powered Engines not Motors
An electric spark generalized & fluctuating effort for accelerant
"We can do over 200,000 kW per second on larger jet aircraft. With a concord set up we void fire - explosion variables through our Emergency Safety System meeting 110 mW (megawatts)"
WHAT WE HAVE
A junk-jet prototype sh*t & one new jet for demonstrations
MORE DETAILS
FLIGHT TIMES
Add extra time for boarding & landing after take off & taxiing then luggage
4 hours or 4.5 hours
A Mach 2 flight from Zurich to Denver takes approximately 3 hours and 45 minutes to cover the 5,159-mile (8,303 km) distance at twice the speed of sound (about 1,320–2,125 km/h depending on altitude/temperature).
1.5 to 2 hours
A Mach 2 flight from Calgary to Toronto takes about 1 hour and 15 minutes, covering a distance of roughly 2,700 kilometers at twice the speed of sound (about 2,450 km/h).
25 - 45 minutes
There are no commercial Mach 2 supersonic flights from North Bay (YYB) to Toronto (YTZ/YYZ), but at Mach 2 (about 2,450 km/h or 1,520 mph), the direct 302 km trip would take roughly 7.5 minutes in the air.
Sydney Nicola Bennett's C/M design voids concerns & upscales passenger & cargo safety at Zero Emissions + Zero Fuel
COST CONTROLS ON MANUFACTURING & MAINTENANCE
Material choices. Shell & exo-shell similar to concord yet different
Likely $25 Million - $40 Million per unit in production with test jets repurposable taking from refurbished junk yard bits
"We can offer scalable sizing offerings with Mach 2 driving costs - price"
The Concorde jet has an overall length of 203 feet 9 inches (62.1 meters) and a fuselage external width of 9 feet 6 inches (2.9 meters).
Dimensions and Size Details
Length: 203 ft 9 in / 61.66–62.1 m (note: the metal airframe stretched 6 to 10 inches during supersonic flight due to heat)
Fuselage Width (External): 9 ft 5 in to 9 ft 6 in (2.88–2.9 m)
Cabin Width (Internal): Approx. 8 ft 7 in (2.63 m)
Wingspan: 83 ft 8 in to 84 ft (25.5–25.6 m)
Height: 37 ft 1 in to 40 ft (11.3–12.2 m)
The length of the Boeing 777X family varies by variant: the Boeing 777-9 is 251 feet 9 inches (76.72 m) long, and the smaller 777-8 is 232 feet 6 inches (70.86 m) long.
AIRBUS A350 COMPARISONS IN PRICING (2026)
Substantially more expensive & higher maintenance cost based on industry anti-access to supply due to layered factors lifting pricing
The Airbus A350 has a list price of $317 million for the A350-900 and $366 million for the A350-1000. Real-world transaction values range from $150 million to $230 million after standard airline discounts, while monthly lease rates average $1.14 million.
Purchase and Lease Costs
A350-900 List Price: ~$317 million (market transaction value roughly $160 million to $185 million)
A350-1000 List Price: ~$366 million
Monthly Lease Rate: ~$1.14 million for a new A350-900
CONCORDS FAILS VS C/M MACH 2
Jet engines like the Concorde's four Rolls-Royce/SNECMA Olympus 593 turbojets are measured in pounds of thrust or equivalent horsepower rather than direct electrical kilowatts.
At Mach 2 cruise, the total output of 144,000 horsepower equals roughly 107,381 kilowatts (107.4 megawatts) of mechanical power.
Engine and Power Specification
Engine Model: Four Rolls-Royce/SNECMA Olympus 593 turbojets
Thrust per Engine (Takeoff with Reheat): 169.2 kN (38,050 lbf)
Thrust per Engine (Dry/Cruise): Approx. 10,000 lbf at Mach 2
Electrical Generators: Four 60 kVA engine-driven generators per airframe
The F15 Eagle at Mach 2 does not burn up. So we wrap in Eagle features Airplane. Equivlance voiding fire or explosion
The exo-shell effect should void with our Emergency Safety System previously concerns plaguing Mach 2 global travel
"If we can build for under $25 Million we will. European international. USA has a lock on approved aviation & Military Industrial"
EAGLE SKIN
The exterior and structural skin of the F-15 Eagle is made from a mix of aluminum, titanium, and advanced composite materials.
Structural Exterior Breakdown
Aluminum: Forms the primary traditional semi-monocoque fuselage skin, control surfaces, and general airframe framework.
Titanium: Used heavily in high-stress and high-heat areas, including the central fuselage bulkheads and engine attachment zones.
Boron Composites: Used as a skin material over an aluminum honeycomb structure on the tail assemblies (vertical and horizontal stabilizers) to keep rudders thin, lightweight, and extremely rigid.
Fiberglass & Graphite: Applied in select fairings and minor structural panels.
$15 Million will be the lowest base price of all materials are sourced. $45 Million at the highest
C/M WILL VOID BAGGAGE LIMITS MEETING A350 AIRBUS SIMULARITIES
A fin for luggage & wing weighing + Kinetics
Concorde passenger baggage allowance permitted one medium-sized carry-on bag plus a briefcase, and a single checked hold suitcase weighing up to 12 kg (26 lbs). Due to the tight space in the supersonic jet, total baggage limits were much smaller than standard commercial flights.
Carry-On Allowance
Pieces: One medium bag and one briefcase.
Dimensions: Maximum size of 45 x 35 x 20 cm (18 x 14 x 8 inches) per item.
Checked Hold Baggage Allowance
Pieces: One single suitcase.
Weight limit: Maximum of 12 kg (26 lbs).
Dimensions: Maximum size of 55 x 40 x 20 cm (22 x 16 x 8 inches).
The Concorde typically carried a standard capacity of 100 passengers, with structural and seating designs accommodating a range of 92 to 128 maximum passengers depending on the specific airline layout.
Cabin Layout and Seating
Standard capacity: 100 total seats
Front cabin: 40 seats
Rear cabin: 60 seats
Seating arrangement: Four-abreast layout (2-2 configuration) due to the narrow fuselage
Airline Configurations
British Airways: Commonly set up for 92 to 100 passengers
Air France: Commonly configured for 100 passengers
Maximum limit: Up to 128 passengers in high-density layouts, though rarely used in regular service to preserve weight and range
C/M does 90 seats. Luggage is important
LOWER OPERATING COSTS
Costs equivlance on seating Vs initial price + maintenance then operating costs
Crash. Now C/M ironed out 90-99% of variables for crash
The Concorde crashed on July 25, 2000, because runway debris punctured a fuel tank, leading to an intense fire and engine failure. The primary factors involved a metal strip, a burst tire, and a fuel ignition
Key Causes of the Crash
Runway Debris: The Air France Flight 4590 ran over a thin titanium metal strip dropped onto the runway by a Continental Airlines DC-10 that had taken off minutes earlier.
Tire Blowout: The metal strip cut into the Concorde's tire, causing it to violently rupture.
Fuel Tank Rupture: Large pieces of the heavy tire slammed into the underside of the left wing, creating a massive pressure wave that forced fuel tank No. 5 to burst outward from the inside.
Ignition and Fire: Escaping jet fuel ignited—likely from an electrical arc in the landing gear bay—causing a severe fire under the wing that crippled the left engines. Federal Aviation Administration (.gov) +1
Loss of Control: Because the plane had already passed the decision speed (V1) during takeoff, the crew could not safely stop. The aircraft struggled into the air, lost thrust, entered a rapid stall, and crashed into a hotel in Gonesse, France, killing all 109 people on board and 4 on the ground.
PILOT & FLIGHT ATTENDANTS
Pilots earn significantly more than flight attendants, with major airline pilots averaging $200,000+ per year (and senior captains making $300k–$450k+), compared to flight attendants who typically earn a median salary of $68,000 to $78,000 per year.
Pilot Salaries
Pay Structure: Paid hourly based on flight time, aircraft type, and position (Captain vs. First Officer), with guaranteed monthly minimums.
Earning Range: Entry-level regional first officers may start around $50,000–$80,000, while senior captains at major legacy mainline carriers can clear $400,000+ annually.
Training & Requirements: Requires extensive, costly training, commercial licenses, an Airline Transport Pilot (ATP) certificate, and thousands of flight hours.
Flight Attendant Salaries
Pay Structure: Paid an hourly flight rate (calculated from when cabin doors close and the aircraft moves) plus a per diem hourly rate for time spent away from base.
Earning Range: New hires often start around $25–$40 per hour ($30,000–$45,000 total first-year pay), while senior international cabin crew with maximum seniority can reach $90,000+.
Training & Requirements: Requires a high school diploma, customer service background, and specialized safety training provided directly by the airline.
"Don't fret" means do not worry,
do not stress, or relax. Fair wages or fair Union wages with access to supply ratios
CYPRESS MOTORS. CYPRESS MOTOR SPORTS
Mach Speeds in Aviation
Supersonic and hypersonic speeds differ primarily by their speed ranges and the physical behavior of air around a moving vehicle. Supersonic speed ranges from Mach 1 to Mach 5 (faster than sound), while hypersonic speed starts at Mach 5 and above (five times faster than sound).
Speed and Physics
Supersonic (Mach 1–5): Speeds are greater than the local speed of sound. Shock waves form and drag increases sharply, but air acts mostly as a standard compressible fluid. Examples include fighter jets and the historic Concorde.
"C/M altered the concord Engine for EV Electric Electricity intake from Kinetics"
Hypersonic (Mach 5+): Speeds reach five times the speed of sound or higher. Air molecules hit the vehicle so hard that they break apart and turn into plasma. This creates extreme heat that can melt normal metals.
"Rotating detonating Plasma Missiles achieve"
Technology and Design
Materials: Supersonic craft use standard aerospace metals. Hypersonic vehicles require special blunt shapes and heavy heat shields to survive extreme temperatures.
Engines: Supersonic planes use standard jet or afterburning turbojet engines. Hypersonic vehicles require advanced engines like scramjets that manage supersonic combustion.
Usage: Supersonic tech is mature, reliable, and widely used in military aviation and missiles. Hypersonic tech is largely experimental or used for specialized fast-strike missiles and space capsule re-entry.
SUB-SONIC
Below supersonic is called subsonic, meaning speeds slower than the speed of sound (Mach 1, or roughly 761 mph / 1,225 km/h at sea level). Right before reaching supersonic speed, an object passes through the transonic zone, where parts of the airflow are supersonic and parts are subsonic.
Speed Categories Below Supersonic
Subsonic: Speeds below Mach 0.8 or under ~1,125 feet per second (340 m/s), where air flows smoothly around an object without shock waves.
Transonic: Speeds right around the sound barrier (typically Mach 0.8 to 1.2), where mixed subsonic and supersonic airflow occurs.
ASTRO MODERN
A startup named Astro Mechanica is developing a hybrid electric jet engine designed to bring back Concorde-style supersonic travel using ultra-lightweight electric hypercar motors supplied by Helix.
How the Turboelectric Engine Works
Decoupled Design: Traditional jet engines mechanically lock the fan and turbine together. Astro Mechanica uses electric motors to separate the core generator from the compression fan.
Adaptive Modes: The electric-driven compressor shifts behavior across flight stages—acting like a turbofan at low speeds, a turbojet at medium speeds, and a ramjet at high supersonic speeds.
Efficiency Goals: Running on liquid natural gas and electric-assisted compression, the design targets 61% more range than the historical Concorde and lower carbon emissions.
Community Views: Opinions on Reddit are mixed regarding whether this counts as a true hybrid without heavy battery storage, though hot-fire prototypes have already undergone testing.
CONCORDE ENGINES. ALL FOUR
Our efforts to Electricify Concord Engines without fuel use are generally successful while we upscale inefficiencies
Concorde was powered by four Rolls-Royce/Snecma Olympus 593 turbojet engines, featuring variable-geometry air intakes and an afterburning reheat system. Together, they produced up to 152,200 lbs of thrust at takeoff.
Engine Specifications and Design
Type: Anglo-French two-spool turbojet with reheat (afterburner).
Thrust: ~38,050 lbs (180 kN) per engine with reheat at takeoff.
Compressor Stages: 14 total stages split evenly (7 low-pressure, 7 high-pressure).
Efficiency: Achieved a record-setting thermal efficiency of roughly 43% during supersonic cruise (Mach 2).
Operation and Performance
Reheat Usage: Burned extra fuel in the exhaust nozzle specifically during takeoff and when pushing through the sound barrier (transonic acceleration from Mach 0.95 to 1.7).
Supercruise: Once cruising at Mach 2 at 60,000 feet, the afterburners were turned off, and the engines sustained supersonic flight purely on dry thrust.
Variable Air Intakes: Controlled by digital computers to slow and compress incoming supersonic air down to subsonic speeds before it entered the engine compressors.
NEW HYBRID ADAPTATIONS
Concorde's classic jet design is inspiring a new hybrid-electric supersonic engine concept that uses ultra-lightweight electric vehicle (EV) hypercar motors instead of direct jet engines mounted to an EV.
The Hybrid Supersonic Project
The Partnership: US aerospace startup Astro Mechanica is teaming up with British EV motor maker Helix—which supplies high-performance motors for the 2,011-hp Lotus Evija and McMurtry Spéirling fan car.
The Goal: Build a "Duality" turboelectric adaptive engine to solve the severe low-speed fuel inefficiency that plagued the Concorde's Rolls-Royce Olympus 593 turbojets.
How it Works: Electric motors decouple the fan/compressor from the internal turbine core. This lets the engine act like an efficient turbofan at takeoff/subsonic speeds, a turbojet at lower supersonic speeds, and a ramjet past Mach 3.
Timeline: High-altitude and high-speed ground testing are underway, with a first flight targeted for 2027 in a custom propulsion testbed aircraft.
C/M refuses to do a Hybrid due to Emissions yet industry entrants are conceptualizing such
OUR EMERGENCY SAFETY SYSTEM REVIEW
With no fuel as a reserve. If a section of Kinectic Energy Generators not Hydrogen back ups in our No-Fuel effort goes offline the aircraft simply glides slower
This is different from air-brake regenerative designs yet is viable especially if incidents damage areas of aircraft. Smooth take off, glide & landing even if a tire blow-our occurs yet same performance
Ours is essentially a modern Concorde under a design difference to void patent, copyright & trademark concerns
C/M PROPELLED BY BEATS PER MINUTE - SECOND
A simple speaker connected to Kinetic Energy Generators
"Simply turn on the beat. Overlay. Control Thrust. Simple. Partially Automated with Manual overide"
Sydney Nicola Bennett's Kinetic Energy Generators. Perpetual Motion Energy
"An EV Electric Engine is a complex Motor. A Motor is simple"
Eleatic Band Catch end of runway & runway debris monitoring. Aircraft carrier inspired
A flight from London to Tokyo at Mach 2 takes approximately 4 hours and 30 minutes to cover the roughly 9,574 kilometer great-circle distance at a supersonic speed of about 2,160 km/h.
THIS CONCORDE PROJECT WAS BORN AROUND 2012
Sydney Nicola Bennett at CIG was restructu4ing between investigative efforts alongside externals working on ones own portfolio
Bennett had a Honda Civic Sport in 2012 & had picked up Jordan R Bennett to fetch wife Amy Toms Bennett at the Calgary International Airport
"Rewind to 2012. Sydney Nic Bennett picks up Jordan R Bennett in Calgary from a temporary condo while Bennett was investigating at an apartment & waiting to move into a new residence after a temporary option with another rented out managing investmnets & working two positions at one time. The two picked up a pregnant Amy Toms Bennett with her first of three children at the Calgary, International, Airport after they relocated from Northern Ontario's North Bay. Nic was already situated connected to international interests through CIG & K.T UN. Jordan & Amy later connected to a Toronto - Oakville option while Nic had a incredibly busy work - travel schedule with studies"
Everything worked out despite NB-OT Neuro-Labs Neuro-Strike War of 2012-2026 & everything leading up to which Sydney N Bennett & Jordan R Bennett did not appreciate having to work around
Jordan R Bennett like then before Jordan. Sydney N Bennett worked out of Downtown Calgary
FAMILY IN CANADA. ALBERTA - ONTARIO
Chartered Accountant. CPA. 1983 Birth. PWC Canada Partner
Sibling of Sydney Nic Bennett. Jordan R Bennett
www.pwc.com/ca/en/contacts/j/jordan-bennett.html
www.linkedin.com/in/jordanrjbennett
Sydney Nicola Bennett. P.Eng
https://2026featurecig.blogspot.com/2026/08/sydney-nicola-bennett-alpha-health.html
"We are unsure if we can conceal a vertical-horizontal micro-Engine with the four mains for Supersonic Flight allowing different forms of take off & glide landings to void damage to tires - brakes & brake debris yet it is expressed in R&D"
https://devisions2.blogspot.com/2026/07/blog-post_654.html
Michael Bloomberg. The Magazine - Media fu*ker has an approach with a team. Its on the right track aiding Net Zero Aviation
https://boomsupersonic.com/press-release/bloomberg-supersonic-jet
Boeing Concorde in Florida rotting
https://supercarblondie.com/boeings-supersonic-airliner-spent-years-by-florida-roadside/
CONCORD SUPERSONIC BANNING
Concorde was restricted from flying at supersonic speeds over land due to the disruptive sonic boom it produced, which caused widespread noise complaints, rattled structures, and led regulatory bodies like the Federal Aviation Administration to ban commercial supersonic flight over land.
Causes of the Overland Ban
Sonic Booms: Continuous explosive pressure waves created during supersonic flight reached the ground as loud twin booms, mimicking explosions or heavy thunder.
Public Outcry: Early test flights and public demonstrations over populated areas led to broken windows and a massive surge of citizen protests and complaints.
Regulatory Action: The Federal Aviation Administration and other international aviation authorities prohibited civilian aircraft from exceeding Mach 1 over landmasses.
Operational Impact on Concorde
Route Restrictions: Operations were strictly limited to transoceanic routes—primarily regular commercial runs between London/Paris and New York/Washington.
Commercial Limitations: The inability to fly fast over land restricted market expansion and global network profitability, contributing heavily to the jet's eventual unviability and retirement in 2003.
SUPERSONIC SILENCERS
Building a quieter supersonic jet involves shaping the airframe to reduce sonic booms to a soft "thump," replacing old turbojet engines with modern turbofans, and using camera systems instead of protruding cockpit windows. Key projects tackling this include NASA's X-59 QueSST and Boom Supersonic's Overture.
Design Strategies for Noise Reduction
Elongated Needles: A very long, slender nose (up to 30 feet) gives air molecules time to move aside, preventing sharp pressure spikes.
Flat Underbellies: Keeping the bottom of the plane smooth and flat ensures uninterrupted airflow while placing bumps and engine inlets on top to shield the ground from noise.
Windowless Cockpits: Removing the bulky forward canopy prevents unwanted shockwaves, relying instead on high-resolution external camera systems.
Modern Turbofans: Replacing deafening 1970s turbojets with high-efficiency turbofan engines significantly lowers takeoff and subsonic noise.
https://youtu.be/KL8voQWqZW8?si=krWADIJZl7I9w5ro
Hubba Hubba = a early basic form of peacocking
To land the lady & get her in the nudies doing things
https://youtu.be/KL8voQWqZW8?si=3D5-4qCJPWltCiNy
UNDERSTAND AIR MOLECULES
Air molecules take virtually zero time to move aside because they are already zooming around at the speed of sound, parting instantly when anything pushes through them.
How Air Moves
Super-fast speed: At room temperature, air particles zip around at about 500 meters per second (roughly 1,100 miles per hour).
Constant bumping: They crash into each other billions of times every second, changing direction in a tiny random walk.
Instant clearing: Because they are already moving so fast, any new object passing through simply shoves the local cluster aside in a fraction of a microsecond.
When Air Cannot Move Fast Enough
Speed of sound limit: If an object travels slower than sound, the air ahead gets the signal to move out of the way smoothly.
Shockwaves: When an object breaks the sound barrier (like a jet plane), it moves too fast for the leading air molecules to be warned, creating a sudden pile-up called a sonic boom.
The idea that an airplane wing's shape splits air so that the top and bottom portions must meet at the back at the same time is a common misconception known as the equal transit time fallacy. In reality, air parcels split by a streamlined shape do not need to meet up again, and air flowing over the curved top actually moves much faster than the time it takes for air to pass underneath.
Why the "Equal Time" Idea is False
No pairing rule: Air particles passing over the top and bottom of a wing do not have a buddy system or a requirement to rejoin at the trailing edge simultaneously.
Faster top flow: Measurements in wind tunnels show that the air moving over the curved top surface arrives at the back edge much faster than the air traveling along the bottom.
Real lift cause: Lift happens because the wing's shape and angle deflect air downward, creating lower pressure on the top surface and higher pressure on the bottom surface in accord with Newton's laws and fluid dynamics.
Sebaticles are not agreed severence. Paid or unpaid
PROGRESS WITH EXTERIOR WIND-SHIELD & CAMERAS
Success rates:
Elongated Needles: A very long, slender nose (up to 30 feet) gives air molecules time to move aside, preventing sharp pressure spikes.
To Upscale a multi-needle deflector to push molecules away deflecting can shrink the 30 ft sizing down cutting costs
"We than apply. Onto all surfaces & wing area"
An effective forcefield effect to control molecular roll
INDUSTRY RACE TO BRING BACK SUPERSONIC TRAVEL
Key Factors and Findings
The Debris: An official investigation determined a titanium alloy strip shed by a Continental Airlines DC-10 on the runway slashed the Concorde's tire.
The Impact: A heavy piece of rubber struck the underside of the wing, sending a hydraulic shockwave that ruptured a fuel tank and ignited a fierce fire.
Systemic Vulnerabilities: Public and aviation analysis noted that prior tire-burst incidents had occurred during the Concorde's history, yet safety upgrades to reinforce the fuel tanks and wings had been delayed or unfulfilled.
Contributory Elements: Observers and operational reviews highlighted additional weight and a minor tailwind component during takeoff that reduced the performance margin.
The Demise of Supersonic Travel: While the fleet was temporarily grounded and retrofitted with Kevlar tank linings, general public and industry opinion agrees that the crash, combined with rising maintenance costs and the post-9/11 aviation downturn, ultimately sealed the end of the Concorde era.
Aerodynamic Design vs. Low-Speed Visibility
Supersonic Shape: The jet needed a sharp, needle-like nose cone to cut through shockwaves and reduce drag at high speeds.
High Angle of Attack: Because of its delta-wing design, the aircraft had to pitch its nose high up into the air during take-off and landing to stay airborne at low speeds.
Obstructed View: This steep, nose-up angle completely hid the runway from the pilot's forward-facing cockpit windows.
How the Nose Worked
Drooping Action: Hydraulic systems lowered the hinged nose tip down by 5 degrees for taxiing and take-off, and down to 12.5 degrees for final landing approaches.
Retractable Visor: A metal shield called a visor slid down into the nose before the nose itself dipped, uncovering the main window glass for the flight crew.
Return to Streamlined Form: Once the plane climbed away from the airport or finished landing, the nose and visor locked back into a straight, flush position for fast flight.
C/M A. Electric Ducted Fans EDF'S
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