Author: J. A. Suddreth
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
National Altitude Rocket Test Facilities
Author: J. A. Suddreth
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
National Altitude Rocket Test Facilities
Author: J. A. Suddreth
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
The necessity for experimental verification of rocket-engine performance at altitude or near-space conditions has long been recognized in the aerospace industry. Recent spacecraft rocket-engine research and development trends toward higher area ratios, advanced nozzle concepts, and nonequilibrium flow conside ations have made altitude simulation a requirement of development pro- grams. Recause the need for information regarding the capabilities and char- acteristics of altitude test facilities that are suitable for l%id-rocket%- engine operation was recognized, this survey was compiled with the help of representatives of industry and government agencies;% % INTROPUCTION The advent of upper-stage and spacecraft engine-vehicle development pro- grams along with the need for more rigorous performance and reliability data justified the construction of a number of altitude test facilities. The test capabilities of these facilities range from small attitude-control engines to large upper-stage engines. The altitude-simulating systems include simple diffusers coupled to the engine nozzle exit (fig. 1), steam ejector coupled to the engine-driven diffuser (fig. 2), and pumped environmental chambers coupled to a diffuser or ejector system for use during engine firing (fig. 3). Several techniques for vacuum generation exist. In addition to the conventional sys- tems of mechanical pumps and steam boilers for stem% ejectors, there are semi- portable liquid-propellant-driven steam generators.
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
The necessity for experimental verification of rocket-engine performance at altitude or near-space conditions has long been recognized in the aerospace industry. Recent spacecraft rocket-engine research and development trends toward higher area ratios, advanced nozzle concepts, and nonequilibrium flow conside ations have made altitude simulation a requirement of development pro- grams. Recause the need for information regarding the capabilities and char- acteristics of altitude test facilities that are suitable for l%id-rocket%- engine operation was recognized, this survey was compiled with the help of representatives of industry and government agencies;% % INTROPUCTION The advent of upper-stage and spacecraft engine-vehicle development pro- grams along with the need for more rigorous performance and reliability data justified the construction of a number of altitude test facilities. The test capabilities of these facilities range from small attitude-control engines to large upper-stage engines. The altitude-simulating systems include simple diffusers coupled to the engine nozzle exit (fig. 1), steam ejector coupled to the engine-driven diffuser (fig. 2), and pumped environmental chambers coupled to a diffuser or ejector system for use during engine firing (fig. 3). Several techniques for vacuum generation exist. In addition to the conventional sys- tems of mechanical pumps and steam boilers for stem% ejectors, there are semi- portable liquid-propellant-driven steam generators.
National Altitude Rocket Test Facilities
Author: Jack A. Suddreth
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 10
Book Description
The necessity for experimental verification of rocket-engine performance at altitude or near-space conditions has long been recognized in the aerospace industry. Recent spacecraft rocket-engine research and development trends toward higher area ratios, advanced nozzle concepts, and nonequilibrium flow conside ations have made altitude simulation a requirement of development pro- grams. Recause the need for information regarding the capabilities and char- acteristics of altitude test facilities that are suitable for l%id-rocket%- engine operation was recognized, this survey was compiled with the help of representatives of industry and government agencies;% % INTROPUCTION The advent of upper-stage and spacecraft engine-vehicle development pro- grams along with the need for more rigorous performance and reliability data justified the construction of a number of altitude test facilities. The test capabilities of these facilities range from small attitude-control engines to large upper-stage engines. The altitude-simulating systems include simple diffusers coupled to the engine nozzle exit (fig. 1), steam ejector coupled to the engine-driven diffuser (fig. 2), and pumped environmental chambers coupled to a diffuser or ejector system for use during engine firing (fig. 3). Several techniques for vacuum generation exist. In addition to the conventional sys- tems of mechanical pumps and steam boilers for stem% ejectors, there are semi- portable liquid-propellant-driven steam generators.
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 10
Book Description
The necessity for experimental verification of rocket-engine performance at altitude or near-space conditions has long been recognized in the aerospace industry. Recent spacecraft rocket-engine research and development trends toward higher area ratios, advanced nozzle concepts, and nonequilibrium flow conside ations have made altitude simulation a requirement of development pro- grams. Recause the need for information regarding the capabilities and char- acteristics of altitude test facilities that are suitable for l%id-rocket%- engine operation was recognized, this survey was compiled with the help of representatives of industry and government agencies;% % INTROPUCTION The advent of upper-stage and spacecraft engine-vehicle development pro- grams along with the need for more rigorous performance and reliability data justified the construction of a number of altitude test facilities. The test capabilities of these facilities range from small attitude-control engines to large upper-stage engines. The altitude-simulating systems include simple diffusers coupled to the engine nozzle exit (fig. 1), steam ejector coupled to the engine-driven diffuser (fig. 2), and pumped environmental chambers coupled to a diffuser or ejector system for use during engine firing (fig. 3). Several techniques for vacuum generation exist. In addition to the conventional sys- tems of mechanical pumps and steam boilers for stem% ejectors, there are semi- portable liquid-propellant-driven steam generators.
Experimental Investigation in an Altitude Test Facility of Burning of Excess Combustibles in a Rocket Engine Exhaust
Author: Harry E. Bloomer
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 36
Book Description
Rocket Testing and Evaluation in Ground Facilities
Author: John H. Povolny
Publisher:
ISBN:
Category : Stages (Rocketry)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Stages (Rocketry)
Languages : en
Pages : 28
Book Description
Rocket Altitude Test Facilities Register
Author:
Publisher:
ISBN: 9789283504047
Category : Rocket engines
Languages : en
Pages : 74
Book Description
Publisher:
ISBN: 9789283504047
Category : Rocket engines
Languages : en
Pages : 74
Book Description
Altitude Simulation Facilities for Rocket Test Firing
Author: G. D. Westcot
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 9
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 9
Book Description
Altitude Simulation Testing Facility Concepts for Large Liquid-propellant Rocket Engines
Author: F. B. Cyran
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Aerospace Testing
Author: Frank Degnan
Publisher: DIANE Publishing
ISBN: 9780788180811
Category : Technology & Engineering
Languages : en
Pages : 50
Book Description
Reviews the cooperation between NASA & DoD since May 1996 to develop a national perspective on aerospace test facilities. Determines (1) the extent to which NASA/DoD working groups ( alliancesÓ) on major test facilities have been operating on a regular basis, (2) NASA's & DoD's actions in response to a future need to test an engine for new Air Force rockets, (3) whether NASA & DoD prepared a congressionally required joint plan on rocket propulsion test facilities, & (4) whether NASA & DoD are implementing a DoD assessment team's recommendation in March 1997 to jointly manage with NASA certain aeronautical test facilities.
Publisher: DIANE Publishing
ISBN: 9780788180811
Category : Technology & Engineering
Languages : en
Pages : 50
Book Description
Reviews the cooperation between NASA & DoD since May 1996 to develop a national perspective on aerospace test facilities. Determines (1) the extent to which NASA/DoD working groups ( alliancesÓ) on major test facilities have been operating on a regular basis, (2) NASA's & DoD's actions in response to a future need to test an engine for new Air Force rockets, (3) whether NASA & DoD prepared a congressionally required joint plan on rocket propulsion test facilities, & (4) whether NASA & DoD are implementing a DoD assessment team's recommendation in March 1997 to jointly manage with NASA certain aeronautical test facilities.
Pursuit of Power
Author: National Aeronautics Administration
Publisher: CreateSpace
ISBN: 9781493576289
Category : Aerodynamics
Languages : en
Pages : 200
Book Description
The NASA Glenn History Office has undertaken the task of documenting many of its historic facilities. Histories of the Icing Research Tunnel, Plum Brook Reactor Facility, Rocket Engine Test Facility, and Altitude Wind Tunnel have been published. These books demonstrate the significance of each facility to the nation's aerospace community while sharing personal stories of some of the unsung researchers, mechanics, and technicians who performed groundbreaking research and made the giant facilities run. It is hoped that this publication continues this tradition. The NASA Glenn History Office has undertaken the task of documenting many of its historic facilities. Histories of the Icing Research Tunnel, Plum Brook Reactor Facility, Rocket Engine Test Facility, and Altitude Wind Tunnel have been published. These books demonstrate the significance of each facility to the nation's aerospace community while sharing personal stories of some of the unsung researchers, mechanics, and technicians who performed groundbreaking research and made the giant facilities run. It is hoped that this publication continues this tradition. This publication documents the Propulsion Systems Laboratory No. 1 and 2 prior to their demolition.
Publisher: CreateSpace
ISBN: 9781493576289
Category : Aerodynamics
Languages : en
Pages : 200
Book Description
The NASA Glenn History Office has undertaken the task of documenting many of its historic facilities. Histories of the Icing Research Tunnel, Plum Brook Reactor Facility, Rocket Engine Test Facility, and Altitude Wind Tunnel have been published. These books demonstrate the significance of each facility to the nation's aerospace community while sharing personal stories of some of the unsung researchers, mechanics, and technicians who performed groundbreaking research and made the giant facilities run. It is hoped that this publication continues this tradition. The NASA Glenn History Office has undertaken the task of documenting many of its historic facilities. Histories of the Icing Research Tunnel, Plum Brook Reactor Facility, Rocket Engine Test Facility, and Altitude Wind Tunnel have been published. These books demonstrate the significance of each facility to the nation's aerospace community while sharing personal stories of some of the unsung researchers, mechanics, and technicians who performed groundbreaking research and made the giant facilities run. It is hoped that this publication continues this tradition. This publication documents the Propulsion Systems Laboratory No. 1 and 2 prior to their demolition.