Author: Joseph F. WasserbauerPublisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32
Book Description
Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Author: Joseph F. WasserbauerPublisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32
Book Description
Performance of Small (100-lb Thrust) Rocket Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Author: Joseph F. WasserbauerPublisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
An investigation was conducted on a small (approximately 100-lb thrust) rocket using coaxial injection of N2H4 and N204. Characteristicvelocity efficiencies of 94% of the theoretical shifting equilibrium value were obtained at a chamber pressure of about 300 psi using a 21tube injector and a combustion chamber characteristic length of 10 inches. Performance at lower chamber pressures could be improved by reducing contraction ratio and thereby increasing the combustion chamber length and injector pressure drop, which would tend to promote better mixing. Calculations based on experimental data showed a vacuum specific impulse of 305 sec. with a nozzle area ratio of 50. (Author).
Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Author: Joseph F. WasserbauerNASA Technical Note
Author: Comparison of Hydrazine Nitrogen Tetroxide and Hydrazine Chlorine Trifluoride in Small Scale Rocket Chambers
Author: R. James RollbuhlerPublisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
Book Description
Applied Mechanics Reviews
Author: U.S. Government Research Reports
Author: Handling Hazardous Materials
Author: D. R. CloydPublisher:
ISBN:
Category : Chemicals
Languages : en
Pages : 106
Book Description
Cumulative Title Index to United States Public Documents, 1789-1976
Author: Daniel W. LesterPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 774
Book Description
Author: James F. Connors