Modular pile-up six way rocket
(up, down, left, right, forward, backward)
Nozzles burn biofuel/oxidizer or compresses air oxidizer in.
Sandaerocopters/Sandaerockets can be attached on the inside and/or outside corners of larger Sandaerocopters, Sandaerockets or Sandaeroships.
external/internal
microwave/laser/gaser
heat of air and/or fuel
Carbon Composite
Quantum Rocket
Vacuum
LaserPipe Rocket
LaserMaser
QUANTUM ROCKET uses Molecules, Atoms, Electrons, Photons and/or Gravitons, expelling them backward to move forward and to create quasi-vacuum to accelerate forward move. Photonic internal/external microwave/laser can heat air (atmosphere gas) when available and/or internal liquid to gas fuel. External quantum can be transmitted by external network such as Sandaeronet (microwave/photons), Solaser (laser/photons) and/or Uniqua (gaser/gravitons). Gives rocket unlimited range when added to quantum pressure impulse (mirror/laser/photons, plasma/gaser/gravitons), after initial impulse, entering a laser and/or gaser highway. External/internal Maser (molecules propelled or combusted), Easer (electrons), Laser (photons) and/or Gaser (gravitons) can clear atmosphere (quasi-vacuum) in front/rear, including Sandaeropipes, circular, spiral and/or straight configurations. Any-matter photo/electric PLASMA Quantum Rocket.
QUANTUM VACUUM or quasi-vacuum can be also molecular, atomic (ionic), electronic, photonic and gravitonic with direct correlation with potential of acceleration of a Quantum Rocket with the highest speed being achieved by a gravitonic vacuum (black hole) and gravitonic rocket/sail (gaser). Space is a quantum field that can be propelled and/or vacuumed through.
QUANTUM ENERGY, molecular, atomic (ionic), electronic, photonic and gravitonic, can come from interior and/or exterior of the rocket/vehicle.
LASER ROCKET shifts from absorbing laser heat to reflecting laser impulse to potential speed of light: Sandaeroship can make power transition from buoyancy, propellers, fuel/air heat maser-laser rocket to mirror laser impulse in Solaser Spaceway. Laser-rocket-sail-space-ships use Solaser external lasers to gain atmosphere/gravity/space fuel acceleration, then as photonic pressure on mirror sail for space acceleration towards light speed. Geosync orbit or polar Solaser allow ground/space laser-rocket sync. Mini/Micro/Nano bio-cyber ships can carry self macro replicating Life and Structures. Sandaerocket laser at atmosphere and gravity level the laser heats initially buoyant and fuel cell hydrogen to plasma rocket to then once atmosphere and gravity is cleared to become reflective propulsive. Graphene/aerographene have nano holes then nanotube maze that maximizes impulse, while allowing light/heat to exit on the other end minimizing damage. Solaser has Solar laser mirrors/lenses. Vacuum formed photonic crystals can be added to vacuum formed graphene and aero-graphene to form mini-macro spaceships.
WATER ROCKET electric heat turns water to vapor, electrolysis turns vapor to hydrogen and oxygen that can recombine in combustion and/or reach plasma with interior and/or exterior photonic laser heating and exhaust impulse. Solaser Network (Sandaerolaser, Sandaeropipe/LaserPipe) can produce H2 as energy battery/fuel/plasma/exhaust impulse from H2O. Electrons/Photons lower heat can accelerates H2O electrolysis or higher heat can generate plasma break off: Electricity/Laser+2H2O=2H2+O2=Impulse.
Laser Pipe Rocket Impeller/laser circular formation heats/pumps in external gas (air, vapor, hydrogen), plasma exits side rockets, adding external energy, matter, reducing gas resistance/attrition and adding mirror-laser impulse post-gravity/atmosphere.
Exterior Laser-Pipe creates molecular vacuum outside rocket, interior Laser-Pipe sends heated gas in, laser heats gas, rocket expels plasma, mirror shuts exhaust when atmosphere/gravity cleared, laser-mirror accelerates Laser-Rocket. Land-Atmo-Geo Laser-Pipes orbital stations after Laser-Rocket flies through maintain rotating sequence of Laser impulse as Earth rotates relative to unidirectional Laser-Rocket. Venus-Earth-Moon-Mars Laser Highway add/sustain acceleration to potential light speed.
ELECTRIC ROCKET, e-rocket, uses electric energy to microwave any gas, as air, to blast plasma backward to achieve forward movement and/or electric to light/mirror photonic laser.
ROCKET CAR, Rcar module, uses water photo-electrolysis hydrogen+oxygen rocket or electric microwave/laser gas plasma e-rocket acceleration, electric linear motor acceleration, laser quasi-vacuum and laser mirror pressure acceleration, in a laser pipe (Sandaeropipe/laser), carbon composite pipe/tunnel, at highest horizontal Sandaerotrain air level, vertical Sandaerovator/tower/pyramid or underground/water tunnel.
Specialized rocket-only module that can be combined with other Sandaeorockets, Sandaerocopters (multicopter-only) and/or Sandaeroships (hybrid multicopter-rocket-airship). Sandaerocopters or Sandaerockets can be attached on the inside and/or outside corners of larger Sandaerocopters, Sandaerockets or Sandaeroships. Modules can be piled up vertically like a traditional rocket or in a pyramid configuration for a single stage or multi-stage launch and carry any quantity of cargo and/or passengers to any distance. Each module carries biofuel tank (ethanol/methanol), oxydizer tank (air/oxygen), air compressor and six way rocket nozzels to burn biofuel/oxidizer and compress air in opposite nozzle.
The bottom nozzle burns fuel/oxydizer until it has only enough to detach and return/manuever to launch site. The top/side nozzles collects and compress air on ascention. The rocket vertical ascention reaches a stationary position at orbital altitude to then ignite side rockets to reach orbital/escape velocity with no air resistance. Uses less fuel/oxydizer, can carry unlimited payloads/passengers with multi modules to any distance and is reusable/maneuvarable using six way nozzles (up/down, left/right and front/back). Maneuvarable hot (fuel+oxidizer) or cold rocket (oxidizer/air).
LaserPipe
Plasma
Gas
Rocket
Impeller
Heat is energy and must feed propulsion of pro-rocket going up and retro-rocket going down. The structure must not be stressed and speeds must have inversed proportion to the atmo density. Modular Omni directional rockets as Sandaerocket. Using what could be retro fuel as coolant is a waist and stress to structure. H2 serves as buoyant propulsion, fuel cell electric propulsion, pro and retro rocket propulsion, attrition and laser heated plasma propulsion.