Author: R. Earl Good
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
The technique of upper atmosphere measurements by analyzing the chemiluminescence of nitric oxide trails deposited by rockets was investigated using wind tunnel simulation. The nitric oxide was released from a model into the low density tunnel flow which had been partially dissociated upstream of the plenum chamber by microwave discharge. The radiant power produced was measured separately by photographic and photoelectric techniques under controlled nitric oxide and atomic oxygen concentration flow rates. The tests were conducted at Mach number 3.4 and at freestream pressures between 1 and 10 microns Hg. The geometric shape of the radiating mixing layer contained between two shockwaves was observed and described in terms of the flow rates. The chemiluminescent NO + O to NO2 + photon reaction rate measured by two independent techniques was found to be k = 3 (plus or minus 2) x 10 to the -12th power cu cm/molecules/seconds. Scaling laws were developed to relate the radiant power to the concentration flow rates. These scaling laws were then used to determine the absolute oxygen concentrations in the upper atmosphere from previously conducted flight experiments. Excellent agreement was obtained between the densities obtained by the nitric oxide release technique and mass spectrometer measurements. (Author).
A Wind Tunnel Investigation of the Nitric Oxide-oxygen Atom Reaction
Author: R. Earl Good
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
The technique of upper atmosphere measurements by analyzing the chemiluminescence of nitric oxide trails deposited by rockets was investigated using wind tunnel simulation. The nitric oxide was released from a model into the low density tunnel flow which had been partially dissociated upstream of the plenum chamber by microwave discharge. The radiant power produced was measured separately by photographic and photoelectric techniques under controlled nitric oxide and atomic oxygen concentration flow rates. The tests were conducted at Mach number 3.4 and at freestream pressures between 1 and 10 microns Hg. The geometric shape of the radiating mixing layer contained between two shockwaves was observed and described in terms of the flow rates. The chemiluminescent NO + O to NO2 + photon reaction rate measured by two independent techniques was found to be k = 3 (plus or minus 2) x 10 to the -12th power cu cm/molecules/seconds. Scaling laws were developed to relate the radiant power to the concentration flow rates. These scaling laws were then used to determine the absolute oxygen concentrations in the upper atmosphere from previously conducted flight experiments. Excellent agreement was obtained between the densities obtained by the nitric oxide release technique and mass spectrometer measurements. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
The technique of upper atmosphere measurements by analyzing the chemiluminescence of nitric oxide trails deposited by rockets was investigated using wind tunnel simulation. The nitric oxide was released from a model into the low density tunnel flow which had been partially dissociated upstream of the plenum chamber by microwave discharge. The radiant power produced was measured separately by photographic and photoelectric techniques under controlled nitric oxide and atomic oxygen concentration flow rates. The tests were conducted at Mach number 3.4 and at freestream pressures between 1 and 10 microns Hg. The geometric shape of the radiating mixing layer contained between two shockwaves was observed and described in terms of the flow rates. The chemiluminescent NO + O to NO2 + photon reaction rate measured by two independent techniques was found to be k = 3 (plus or minus 2) x 10 to the -12th power cu cm/molecules/seconds. Scaling laws were developed to relate the radiant power to the concentration flow rates. These scaling laws were then used to determine the absolute oxygen concentrations in the upper atmosphere from previously conducted flight experiments. Excellent agreement was obtained between the densities obtained by the nitric oxide release technique and mass spectrometer measurements. (Author).
Upper Atmosphere O-atom Densities by Wind Tunnel Simulation of Nitric Oxide Releases
Author: D. Golomb
Publisher:
ISBN:
Category : Nitric oxide
Languages : en
Pages : 8
Book Description
Publisher:
ISBN:
Category : Nitric oxide
Languages : en
Pages : 8
Book Description
NO-O Chemiluminescent Reaction in a Low-density Wind Tunnel
Author: F. P. Delgreco
Publisher:
ISBN:
Category : Chemiluminescence
Languages : en
Pages : 10
Book Description
Nitric oxide was injected into a supersonic stream of air containing atomic oxygen in a low density wind tunnel. A photon emission rate was measured in the reaction zone of 3 x 10 to the -12th power cc/sec which is higher by 4-5 orders of magnitude than observed in "ordinary" laboratory flow tubes. This confirmed observations during upper atmosphere releases of nitric oxide.
Publisher:
ISBN:
Category : Chemiluminescence
Languages : en
Pages : 10
Book Description
Nitric oxide was injected into a supersonic stream of air containing atomic oxygen in a low density wind tunnel. A photon emission rate was measured in the reaction zone of 3 x 10 to the -12th power cc/sec which is higher by 4-5 orders of magnitude than observed in "ordinary" laboratory flow tubes. This confirmed observations during upper atmosphere releases of nitric oxide.
NO-O Chemiluminescent Reaction in a Low-density Wind Tunnel
Author: F. P. Delgreco
Publisher:
ISBN:
Category : Chemiluminescence
Languages : en
Pages : 0
Book Description
Nitric oxide was injected into a supersonic stream of air containing atomic oxygen in a low density wind tunnel. A photon emission rate was measured in the reaction zone of 3 x 10 to the -12th power cc/sec which is higher by 4-5 orders of magnitude than observed in "ordinary" laboratory flow tubes. This confirmed observations during upper atmosphere releases of nitric oxide.
Publisher:
ISBN:
Category : Chemiluminescence
Languages : en
Pages : 0
Book Description
Nitric oxide was injected into a supersonic stream of air containing atomic oxygen in a low density wind tunnel. A photon emission rate was measured in the reaction zone of 3 x 10 to the -12th power cc/sec which is higher by 4-5 orders of magnitude than observed in "ordinary" laboratory flow tubes. This confirmed observations during upper atmosphere releases of nitric oxide.
Simulation of Chemiluminescent Reaction of Nitric Oxide with Atomic Oxygen in a Supersonic Low Density Wind Tunnel, Part Ii
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Low density wind tunnel tests were carried out at Mach 2 and 3 to simulate the release of nitric oxide in the upper atmosphere from a sounding rocket. The supersonic flow contained atomic oxygen, and the wall-less chemiluminescent reaction of O with NO was investigated. Reaction rate constants thus obtained were up to 5 orders of magnitude higher than previously obtained laboratory rate constants. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Low density wind tunnel tests were carried out at Mach 2 and 3 to simulate the release of nitric oxide in the upper atmosphere from a sounding rocket. The supersonic flow contained atomic oxygen, and the wall-less chemiluminescent reaction of O with NO was investigated. Reaction rate constants thus obtained were up to 5 orders of magnitude higher than previously obtained laboratory rate constants. (Author).
Simulation of Chemiluminescent Reaction of Nitric Oxide with Atomic Oxygen in a Supersonic Low Density Wind Tunnel
Author: Jan A. VAN DER Bliek
Publisher:
ISBN:
Category :
Languages : en
Pages : 68
Book Description
Low density wind tunnel tests were carried out at Mach 3 to simulate the release of nitric oxide in the upper atmosphere from a sounding rocket. The supersonic flow contained atomic oxygen, and the chemiluminescent reaction of O with NO was investigated. This interim report presents some of the details of the experimental arrangement and preliminary results of the first test series. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 68
Book Description
Low density wind tunnel tests were carried out at Mach 3 to simulate the release of nitric oxide in the upper atmosphere from a sounding rocket. The supersonic flow contained atomic oxygen, and the chemiluminescent reaction of O with NO was investigated. This interim report presents some of the details of the experimental arrangement and preliminary results of the first test series. (Author).
Oxygen Atom Determination in the Upper Atmosphere by Chemiluminescence of Nitric Oxide
Author: D. Golomb
Publisher:
ISBN:
Category : Air Force Cambridge Research Laboratories (U.S.)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Air Force Cambridge Research Laboratories (U.S.)
Languages : en
Pages : 32
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 776
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 776
Book Description
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1078
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1078
Book Description