[Joe] is well known for his thrust-vectoring rockets, some of which have came within a hair’s breadth of making a perfectpowered landing. Previous rockets have usedlarger, more complex flight computers, but for this round, he wanted to go as small and minimalist as possible. Each stage ...
Thrust vectoring enhances aircraft and spacecraft maneuverability. The propulsion systems of aircraft, using gas turbine engines, and spacecraft, using solid or liquid rockets, generate compressed gases that are directed through a nozzle to generate forward thrust. This patent describes opening ports to...
A two-stage secondary-flow jet-based fluidic thrust vectoring nozzle is developed to achieve a greater fluidic vector deflection angle based on the single-stage jet fluidic thrust vector control. The principle is to deflect the primary flow once more following the initial deflection, demonstrating th...
thus providing four aerofin control axes and the two-axes omni-directional TVC. The direct linkage system between the aerofins and the TVC causes the thrust and the aerofins to assist each other in changing the direction of the missile. When the aerofins go into a roll mode (i.e., the...
Check out the results in the video below. Some attempts to reduce the number of rotors work better than others, of course, but this worked out great, and we’re looking forward to the promised improvements to come. Continue reading “Single-Rotor Drone: A Thrust-Vectoring Monocopter” → ...
Strykowski PJ, Krothapalli A, Forliti DJ (1996) Counterflow thrust vectoring of supersonic jets. AIAA J 34(11):2306–2314 Google Scholar Hunter CA, Deere KA (1999) Computational investigation of fluidic counterflow thrust vectoring, AIAA 99-2669. In: 35th AIAA/ASME/SAE/ASEE joint propulsion...
Main objective of this paper is to determine the optimum nozzle parameters for various configuration of Thrust vectoring Nozzle. Various Thrust Vectoring systems are Gimbaled, Jet Vane, and Jet Tab etc. Because, these thrust vectoring systems are being used in Rockets and Missiles.D.Daljit Majil...
The rocket considered in this study is equipped with a single motor, so the thrust vectoring allows the control of the motion in the pitch–yaw angle without any effect on the roll motion. The analysis considers the pitch angle as the only measured system output. The design requirements for ...
The rocket considered in this study is equipped with a single motor, so the thrust vectoring allows the control of the motion in the pitch–yaw angle without any effect on the roll motion. The analysis considers the pitch angle as the only measured system output. The design requirements for ...
The kind of actuator assumed in the study is used in space rockets due to the fact that it can operate in the vacuum of space, where classical aerodynamic control surfaces cease to be effective. Jenie et al. [27] investigated the control of the Falcon 9 rocket using thrust vectoring. The...