The launch will be very cheap at a projected cost of $1鈥 5/lb. The cable is made from cheap artificial fiber widely produced by modern industries.Alexander A. Bolonkin Dr. Sci.Non-Rocket Space Launch and Flight
Pre-Launch: 3 FaceBook tools you need to set up before you launch your store The social media setup you need for a successful launch The crucial social media tool that will save you hundreds of hours How to use coupons to rocket your store’s growth Why email is critical for your sales...
Reusable rocket technology and other propulsion system developments have made space travel more affordable and practical, enabling more frequent flights and discoveries. Having a thorough understanding of the origins of the universe and the potential for extraterrestrial life will come from the exploration ...
Non-Rocket Space Launch and Flight accelerator, tether system, Sun and magnetic sails, solar wind sail, radioisotope sail, electrostatic space sail, laser beam, kinetic anti-gravitator (rep... AA Bolonkin 被引量: 124发表: 2005年 The potential of inorganic mass spectrometry in mineral and trace...
Application of Combustion Stabilization Devices to Liquid Rocket Engine Application of combustion stabilization devices such as baffle and acoustic cavity to liquid propellant rocket engine is investigated to suppress high-frequency combustion instability, i.e., acoustic instability. First, these damping dev...
5.The propulsion system according to claim 1, wherein said engine has a nozzle with an entrance and said at least one rocket is positioned at said nozzle entrance. 6.The propulsion system according to claim 1, wherein said engine has a nozzle and said at least one rocket is positioned so...
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Tehiru Technologies’ hybrid, modular, cost-efficient air-launched rocket propulsion system uses electric landing, and is reusable and sustainable. CrystalEn is developing a technology that enables the growth of single-crystal diamonds to build next-generation materials for the semiconductor industry. C...
This study is based around maximizing the performance of an airbreathing 2nd stage Winged Cone Vehicle, as part of a three-stage rocket-scramjet-rocket launch system for payload masses of the order of 100kg. The concept of a minimum trim vehicle is introduced, where it is desired to alter ...