Article Interstellar Flight 5 2 16 AFTER RBC DOI 10.32370/2018_07_17 Flight of Outer Solar System Alexander Bolonkin C&R,
[email protected] Abstract Author researches, discusses and estimates the need parameters of launch systems the mini automatic probe for flight to the nearest star systems “Alpha-Centauri” and others. He shows that problem is very difficult for current and future technology. Launch requests gigantic energy, expensive equipment and large trip time. The conventional nuclear and thermonuclear on-board reactors cannot also solve this problem (Part 1). Author offers and researches three new possible perspective propulsion systems: multi-reflex light system used new sell-multi-reflex mirror and lasers (Part 2); cold plasma beam from Earth (Part 3) and on-board Micro Black Hole (MBH) nuclear photon rocket (Part 4). In all methods, he offered innovations, which make possible to implement all with current technology. Two first methods request the high altitude (40 ÷ 80 km) mast. He estimates: the requested launch system (laser multi-reflect propulsion, cold plasma beam propulsion, MBH nuclear propulsion, etc.);grown and board equipment, energy installation (generator and accelerator); interstellar flight; environmental, medium drag; interstellar micro particles; communication with Earth. Author showed – the most realistic interstellar launch system is laser beam used the cell reflective mirror or ultra-cold plasma beam. Keywords: interstellar launch, interstellar flight, interstellar propulsion and generator systems, laser beam, cell mirror, laser propulsion, plasma beam propulsion, photon rocket, micro black hole generator. Contents Introduction. Review of main problem an interstellar flight. Part 1. Research of Space Flight in Outer Solar System.