Discarding Old Rocket Motors

SPACE1 is Discarding a Cache of Old Obsolete Rocket Motors
In with the new, out with the old. Old rocket motors are now replaced with the new ELECTRO DYNAMIC GALAXY CLASS SAFETY ROCKET PROPULSION SPACESHIP & SPACECRAFT system. Therefore SPACE1 has a surplus of the obsolete conventional rocket-fuel-based mechanical rocket motors and is liquidating the entire lot.

We've come a long way, and rocket engines at SPACE1 have collected over a period of seven years, each design evolving into vestibules of greater and greater impulse thrust efficiency over the time span. Storage space is at a premium these days as the space complex and launch centers  have fully expanded, and the lot of engines must go. For avid aeronautical engineers, old engines can undergo refurbishing for new life and work their way into the current slew of modern day rockets and spacecrafts. It's a task left for keen rocket enthusiasts wanting to take advantage of mere pennies on the dollar. For more information and to buy the lot of old rocket engines, contact SPACE1 founder and owner Humanoido through SPACE1 Corporate Headquarters.

From the beginning of the founding of SPACE1, Humanoido has engineered copious quantities of rocket engines by assembly line for space flight, quickly testing and evolving their designs for the continual emergence of new invented rocket designs and spacecraft. Humanoido has searched far and wide to acquire the exact needed rocket engine parts, making the best of domestic and international sources as far away as China.

Space1 Rocket Engine Reliability

It took five F-1 rocket engines on the Saturn 5 Moon rocket, but the complexity and expense was astronomical. SPACE1 uses a simplified and reliable one engine with the power for space travel.

Illustration by Nasa showing main parts of the
F-1 rocket engine as used during the Apollo program.

Making Rocket Engines Safe
It seems there is no limit of the number of rocket engines that space companies are willing to put on their rockets. However, as the number of rocket engines increase, so does the risk of failure. This increases the need for redundancy and more engines to compensate for potential engine failures.

— SPACE1 is the only space industry, private or otherwise, which has the original Safety Rocket. It you plan to go up into space, tour the final frontier, or relocate off-planet, be sure to choose the reliability of a Safety Rocket if human life is valued. —

SPACE1 uses the HRE Herculean Rocket Engine which can undergo rapid printing for ease of manufacturing. With a printer on the Moon or Mars, engines could be rapidly printed to build up a Lunar and Martian base fleet of rockets. The HRE aces functioning with no moving parts, thus making the system ultimately dependable and reliable.

In the design, the nozzle is dimensioned for the most effective functioning and engineered for the absence of degradations such as errant harmonics and vibrations. One size fits all makes the most effective rocket engine with easy interfacing. The Herculean engine has a case history of no failures and 100% reliability. SPACE1 rockets utilize only one HRE given that its thrust ratio power has satisfied all the needs of space travel. HRE uses Patonic fuel which can be manufactured on other worlds or gathered in its free hydroxylated form on the Earth.

Space1 Rocket Fuel for Super Rocket X

SPACE1 Rocket Engine Simplified

Space1 Massive Herculean Engine Approved

Space1 Hurculean Rocket Engine

Space1 Herculean Safety Rocket Engine Invention

The complexity of the Apollo F-1 is outlined by NASA as follows:
The F-1 engine has a complex ignition sequence which will be described here.  First, a description of the engine. A large combustion chamber and bell have an injector plate at the top, through which RP-1 fuel and LOX are injected at high pressure. Above the injector is the LOX dome which also transmits the force of the thrust from the engine to the rocket's structure. A single-shaft turbopump is mounted beside the combustion chamber. The turbine is at the bottom and is driven by the exhaust gas from burning RP-1 and LOX in a fuel-rich mixture in a gas generator. After powering the turbine, the exhaust gases pass through a heat exchanger, then to a wrap-around exhaust manifold which feeds it into the periphery of the engine bell. The final task for these hot gases is to cool and protect the nozzle extension from the far hotter exhaust of the main engine itself. Above the turbine, on the same shaft, is the fuel pump with two inlets from the fuel tank and two outlets going, via shut-off valves, to the injector plate. A line from one of these 'feeds' supplies the gas generator with fuel. Fuel is also used within the engine as a lubricant and as a hydraulic working fluid, though before launch, RJ-1 ramjet fuel is supplied from the ground for this purpose. At the top of the turbopump shaft is the LOX pump with a single, large inlet in-line with the turboshaft axis. This pump also has two outlet lines, with valves, to feed the injector plate. One line also supplies LOX to the gas generator. The interior lining of the combustion chamber and engine bell consists of a myriad of pipework through which a large portion of the fuel supply is fed. This cools the chamber and bell structure while also pre-warming the fuel. Lastly, an igniter, containing a cartridge of hypergolic fluid with burst diaphragms at either end, is in the high pressure fuel circuit and has its own inject point in the combustion chamber. This fluid is triethylboron with 10-15% triethylaluminium. At T minus 8.9 seconds, a signal from the automatic sequencer fires four pyrotechnic devices. Two of them cause the fuel-rich turbine exhaust gas to ignite when it enters the engine bell. Another begins combustion within the gas generator while the fourth ignites the exhaust from the turbine. Links are burned away by these igniters to generate an electrical signal to move the start solenoid. The start solenoid directs hydraulic pressure from the ground supply to open the main LOX valves. LOX begins to flow through the LOX pump, starting it to rotate, then into the combustion chamber. The opening of both LOX valves also causes a valve to allow fuel and LOX into the gas generator, where they ignite and accelerate the turbine. Fuel and LOX pressures rise as the turbine gains speed. The fuel-rich exhaust from the gas generator ignites in the engine bell to prevent backfiring and burping of the engine. The increasing pressure in the fuel lines opens a valve, the igniter fuel valve, letting fuel pressure reach the hypergol cartridge which promptly ruptures. Hypergolic fluid, followed by fuel, enters the chamber through its port where it spontaneously ignites on contact with the LOX already in the chamber. Rising combustion-induced pressure on the injector plate actuates the ignition monitor valve, directing hydraulic fluid to open the main fuel valves. These are the valves in the fuel lines between the turbopump and the injector plate. The fuel flushes out ethylene glycol which had been preloaded into the cooling pipework around the combustion chamber and nozzle. The heavy load of ethylene glycol mixed with the first injection of fuel slows the build-up of thrust, giving a gentler start. Fluid pressure through calibrated orifices completes the opening of the fuel valves and fuel enters the combustion chamber where it burns in the already flaming gases. The exact time that the main fuel valves open is sequenced across the five engines to spread the rise in applied force that the structure of the rocket must withstand. The thrust [rises] during the start-up of each engine. It takes two seconds for full performance to be attained on all engines once the first has begun increasing. The engines are started in a staggered 1-2-2 sequence so that the rocket's structure would be spared a single large load increase, with the centre engine being the first to start. The outboard engines exhibit a hiccup in their build-up due to the ingestion of helium from the pogo suppression system installed in each one. The centre engine does not have this installed. As the flow of fuel and LOX rises to maximum, the chamber pressure, and therefore thrust, is monitored to confirm that the required force has been achieved. With the turbopump at full speed, fuel pressure exceeds hydraulic pressure supplied from ground equipment. Check valves switch the engine's hydraulic supply to be fed from the rocket's fuel instead of from the ground.

Space1 Rocket Fuel Injection & Potonic Hydroxil Acid

Obsolete method of rocket engine fuel injection

Space1 has simplified and vastly improved rocket fuel injection on the USS Pioneer rocket which provides a never before seen level of fuel and rocket motor safety. 

The process first involves one very large fuel tank, named the FAT tank, which is part of the powerful S1 engine that takes up most of main embodiment of the rocket. Next, the tank is fitted with the supplanted engine nozzle, a precision static regulatory device with sealant rubber o-rings and no moving parts that controls the thrust vector. 

The NMP concept is prevalent throughout the USS Pioneer, again to control and maintain prevalent safety and reliability. Next, the massive tank is charged with potonic fuel modified hydroxil acid, made extremely potent, by the larger secondary tank which holds the initial fuel in liquid form. Potonic Hydroxil Acid PHA may cause blistering and suffocation so safety is required in the final fuel loaded mixed condition when achieving a charged rocket stage. Next, the secondary largest tank is pressurized and Potonic Hydroxil Acid is valve chambered into the rocket engine. Finally the pumps are activated and oxygen is pumped into the rocket's potonic fuel tank, thus reaching a predetermined level of nominal pressurization. Fueling safety on the launch pad is achieved by maintaining distance from the fuel tank.

Space1 Electric Engine

Space1 Chief Executive Humanoido has given a directive to begin, effectively immediately, a new summer core project changing the fuel of the rocket fleet, which currently contains powerful cyanic compounds that may combust under excessively hot conditions, to that of a cool electric and more safe EM design engine. The EM engines will cluster the rocket minimally to safely propel it skyward at reasonable Gforce. Minimal G forces will lessen the requirements on the astronauts space suit while providing a smoother ride for tourists.

The new fleet will contain electric engines rather than black powder motors used by most rockets currently in boosters today. Black powder is a combustible fuel that loads into the rocket, a design originating from thousands of years ago invented by the Chinese for use in war.

Electric rockets develop powerful thrust over unit time, slower impulse than black powder, but equal in terms of delivery over time. The Gforce will not have the heavy side effects of black powder and thus will create a more comfortable ride into space. "We view the use of the new electric rocket engines to be a safe way to traverse space and safely launch in places with high summer heat. Engines are versatile, reusable and can be maintained and refurbished or replaced."

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Space1 Rocket Engine Bolt On

THE MULTI FOLD ROCKET ENGINE PERFORMANCE BOLT- ON COMPONENT

Humanoido now has a new invention that bolts on to the existing Space1 stock rocket engine in a way that can multi-fold increase engine component  performance. In the long term, this will allow Space1 to use a less costly modified engine and achieve deeper space missions, while standardizing the fleet with one engine design. This can reduce the cost of space travel while creating a faster turn around time from one rocket mission to the next.

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Space1 Hurculean Rocket Engine

HERCULEAN ROCKET ENGINES
Space1 introduces the Herculean Rocket Engine, named after the Greek God Hercules

Space1 has tested a variety of rocket engine designs offering a wide range of size, mass, thrust and time ratios. Rocket dynamics design studies show data for a flux flow ratio that matches the Space1 canister rocket engine specifications.

This new configuration should produce more thrust, in theory. Humanoido, rocket scientist and owner of Space1, is now implementing a modification to the fleet's stock engine, for a fuel ratio with new parameters to gain significant engine performance. Implementing this revision overall will of course require not only engine modifications but also time, design, manufacturing and testing.

Humanoido now has a new invention that bolts on to the existing Space1 stock rocket engine in a way that can multi-fold increase engine performance. In the long term, this will allow Space1 to use a less costly modified engine and achieve deeper space missions, while standardizing the fleet with one engine design. This can reduce the cost of space travel while creating a faster turn around time from one rocket mission to the next.

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Space1 Adiabatic Earth Motor Specifications

Humanoido invented Adiabatic Earth Motor AEM decades ago and now it's getting renewed interest. In the planning are construction projects for building 12 new motors and experimenting with variations on the original design. AEM is expected to have numerous applications in the physics science field and may provide revenue if a smaller version is put on the market.

Humanoido has provided Space1 with the only
Adiabatic Earth Motor AEM. It was air flown
7,600 miles from Humanoido's  Science Laboratory
in the USA to the Taiwan Rocket and Space
Sciences Lab. Earth Motor is an Adiabatic motor 
that can do work by displacing mechanical 
pressure waves, even though the motor is
comprised of an electronic invention. AEM passed
all airport TSA luggage security in the USA and
checkpoints in Japan and Taiwan.

Overview
About the Earth Motor. Basically a motor can do work by generating displacing mechanical pressure waves. This induces a vibratory nature as well as a sound harmonic compression of first and second "mechanical spectral" levels, regions which can be tuned for destructive or constructive interference of waves thus generating nodal points of power. The nodes can yield places of energy or no energy which then can be utilized in real time or collected, recorded and stored. Therefore the motor is capable of sending out or transmitting work to other points in space, but within the confines of a medium. 

Tuning & Calibration
The motor is thus tuned to the pressure, density, and temperature of the medium. This calibration determines the speed of the motor, along with an electronic tuning that adjusts the mechanical frequency of transmitting work. The motor is not electromagnetic in nature, in terms of its transmitted work. However, the motor itself is electronic and driven by CMOS and integrated circuit technology. 

Motor Work & Power Equations
The equation for the work done is the energy transferred from one place to another. The amount of work done is the force times the distance. The motor power is a measure of how quickly work is being done. Power is expressed as work done divided by time taken. Motion of the medium can effect work perform by the motor thus increasing or decreasing its mechanistic speed. Viscosity can also be used to provide motor attenuation.

Penetrating Power
Adiabatic Earth Motor AEM generates power waves that can penetrate and travel through all forms of matter, such as a solid, liquid, gas or plasma stream. The energy carried by the motor's oscillating wave converts back and forth between potential energy of the extra compression or lateral displacement stream (with a transverse function) of matter, and the kinetic energy of the displacement velocity of particles of the medium.

Motor Attributes
The motor does work in a vector from 17m to 17mm. The speed and direction will make up a velocity vector while the wave number and direction create a wave vector. The motor is not isothermal but rather adiabatic.

Periodicy
The periodicy of the motor is yet to be measured but will depend on frequency, amplitude, pressure, speed and direction.

Refraction
If the medium does not have constant physical properties, the motor can be refracted, and either disperse or focus its work. Refraction has potential space-time applications and the ability to splay energy for work to multiple places at the same time from only one AEM motor. Drawing refraction energy does not tax the AEM in any way, therefore maximum draw is allowable from a maximum number of nodals.

Amplification
The original AEM did not have internal amplification. The new AEM has provisions for amplification to significantly increase power. The horsepower will vary with the size of the AEM packaging and the size of the motor.

Motor Speed Equation
The speed of the motor is defined according to the Newton-Laplacian equation c = square root of K/rho where K = elastic bulk modulus, c = sound velocity, rho = density. Therefore the motor speed is proportional to the square root of the ratio of the bulk modulus of the medium to its density.

Motor or Engine?
The difference between a motor and an engine is that motors run on electricity while engines run on combustion.

Space1 Electronic Motor

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Space1 Electronic Motor

The Humanoido Rocket EMotor prototype 
invention was transferred to Space1's 
Taiwan rocket lab

This fascinating electronic EMotor is now ready for rocket development. The futuristic motor can be repackaged to serve conventional or rocket technology.

History
Years ago, the founder of Space1 invented an electronic motor in his American scientific laboratory. A single prototype was manufactured and tested over decades. This prototype was placed in check through luggage, passed TSA airport security and is now at the main rocket lab in Taiwan for analysis of new space applications.

Planning
Space1 is interested in constructing a new schematic diagram, buying parts from the Electronics Part Plaza, and assembling a dozen of the motors for various new applications.

Detail
Some of these new engines may be offered up for sale. They could be offered assembled or in kit form. Assembled units can have specific engine tuning for specific apps. The motor uses basic electronics parts, a PCB, CMOS integrated circuit technology, rheostat tuning, discrete components and is extremely reliable. The motor is battery operated for remote functions and control.

Testing
In harsh tests, the prototype motor survived freezing temperatures down to -40 degrees F. and box heat approaching +120 deg. F. and continued to work. It was also subjected to high levels of humidity and water, vibration, rough handling, and ten-foot drop force tests, again surviving. It passed all corrosive tests over the years and continued to function as designed after being in outdoor conditions for a decade.

Applications
Applications looked at in 2016 and for 2017 include a marketable product, rocket motor, a micro-miniature version, single and multi board motor arrays, parallel phasing, automotive version, various sim apps, harmonics testing, timing applications, and specific devices requiring EMotor technology.

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