Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 212
Book Description
Solid Rocket Thrust Vector Control
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 212
Book Description
Thrust Vector Control Requirement for Launch Vehicles Using a 260-inch Solid Rocket First Stage
Author: Carl J. DanieleAdvanced Solid Rocket Motor Nozzle Thrust Vector Control Flex-seal Development Status
Author: William S. PrinsH-II Solid Rocket Booster Thrust Vector Control System
Author: Eiki IshibashiModeling, and Classical and Advanced Control of a Solid Rocket Motor Thrust Vector Control System
Author: Jackson Hoa-Wai JungPublisher:
ISBN:
Category :
Languages : en
Pages : 248
Book Description
Chamber Gas Secondary Injection Thrust Vector Control for High Performance Solid Rocket Motors
Author: J. R. StevensPublisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
The primary objectives of this program are (1) to demonstrate a thrust vector control (TVC) system optimized for overall propulsion efficiency for advanced upper-stage ICBM rocket motors, and (2) to provide the data and technology necessary for design of future TVC systems. The proposed TVC system is comprised of four poppet valves mounted 90 deg apart on a submerged nozzle. Three nonactuated versions of the submerged hot gas valve were evaluated by static testing. The primary difference between the three designs was the length of the dam enshrouding the centerbody and pintle in the subsonic portion of the valve. (Author).
Proportional Solid Propellant Secondary Injection Thrust Vector Control Study
Author: A Method of Thrust Vector Control for Plug-type Nozzles with Application to Solid Propellant Rockets
Author: Brent William SilverRocket Thrust Vector Control by Jetevator
Author: A. G. ScottHot Gas Secondary Injection Thrust Vector Control Demonstration Program
Author: Carver G. KennedyPublisher:
ISBN:
Category :
Languages : en
Pages : 99
Book Description
This program was established to design, develop, and demonstrate a hot gas secondary injection thrust vector control system (HGSITVC) for large solid propellant rocket motors. Phase I of the program was the design, analysis, and optimization of a 156 in. diameter motor HGSITVC system. The data from this baseline design was used to design four test pintle valves for demonstration on 65 in. diameter test motors. Phase II consisted of designing a four valve, 120 in. diameter motor HGSITVC system using the basic designs and design data developed under Phase I. The 120 in. diameter test motor demonstrated four full scale 156 in. diameter motor pintle valves. The 156 in. diameter motor uses 16 pintle valves of the design tested. (Author).