Aerospace & Defense
Aircraft Wings are placed perpendicular and horizontal; and parallel to the ground; to the fuselage, as can be seen as an standard practice. This placement is basically inspired by body structure of birds. It has its own disadvantage , like excess clearance require on both sides of runways,
Aircraft landing gear and structural components and turbo-machinery components exploited at moderate temperature (“critical components” or “components”) are subjected to severe loading, corrosion, and adverse environmental conditions and they have complex shapes varying from thin to thick sections.
What problem my design idea (called AirView) solves:
The design provides a method of saving lives by avoiding Controlled Flight Into Terrain (CFIT) in any size aircraft, plane or helicopters.
AirView also provides a Functional and Affordable solution for small &
Disruptive Drone Technological Solutions to Develop Safe Night Forest Fire Fighting Capability & Properly Combat CO2 Emissions
The maturity of the technologies for the guidance and control of UASs allows proposing innovative operational options such as the ability to spray a significant amount of an agent of any sort at a pre-established point in the atmosphere.
This is the case of NitroFirex,
Project Developing and Introducing Technology for Large-Size Functional Monocoque (LFM) Fabrication Outside of the Terrestria
Relevance and novelty: for the first time ever, rocket and space equipment production and extraterrestrial macro engineering will be moved off of the Earth. This is like sending the first man into Space.
The prosthesis in 2050 would mean surpassing ordinary human strength. The future belongs to the trans-human and the power of machine integrated human body The US already has plans to bring cyborgs to the military. The future looks very bright for prosthetics.
This space-transportation-system proposal is a reusable, optionally-manned, modular spaceplane to transport payloads and/or personnel into low-earth orbit. The emphasis is to reduce the number of maintenance man-hours vs. flight-hours to drastically reduce 'turn-around' time, making the vehicle commercially viable.
Enters Mars orbit via MAREO II Orbiter (FIGURE THREE; Holmin CTF 2017, 2018). Cone stack launches piggyback atop twin external tanks, six cryo engines, four SRBs. Comprises 33'D base block; aeroshell; stabilizers; aft-canted main engines; adapter ring jettisoning for orbital rendezvous docking; aerobraking bracing strut; revolving wheel habitat;
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