Characteristic sample temperature and pressure during processing of titanium nitride combustion synthesis with liquid nitrogen

1998 ◽  
Vol 33 (10) ◽  
pp. 2573-2576 ◽  
Author(s):  
M Shibuya ◽  
J. F Despres ◽  
O Odawara
2019 ◽  
Vol 220 ◽  
pp. 02005
Author(s):  
Kirill Khorkov ◽  
Dmitry Kochuev ◽  
Anton Chernikov ◽  
Valery Prokoshev ◽  
Sergey Arakelian

In this paper, we present the results of an experimental study of the carbon microcrystals formation by direct laser action on the carbon target surface at temperature of liquid nitrogen. It is demonstrated that the formation of microcrystals occurs in the subsurface layer and is caused by the achievement of critical temperature and pressure.


ChemInform ◽  
2001 ◽  
Vol 32 (9) ◽  
pp. no-no
Author(s):  
R. M. Marin-Ayral ◽  
C. Pascal ◽  
F. Martinez ◽  
J. C. Tedenac

1996 ◽  
Vol 26 (2) ◽  
pp. 1875-1881 ◽  
Author(s):  
K. Brezinsky ◽  
J.A. Brehm ◽  
C.K. Law ◽  
I. Glassman

Author(s):  
A.A. Ustsov ◽  
M.Yu. Kupriyanov

We performed the required theoretical computations to simulate the process of pumping saturated liquid nitrogen vapours, accounting for the assumptions adopted. The paper provides a schematic of the test bench and describes the sequence of experiment stages. We checked whether the storage Dewar and volumetric vacuum pump were selected correctly so as to ensure the required evacuation level above the liquid nitrogen surface. We built our test bench and conducted an experiment involving thermostatting in the 63 to 77 K temperature range, and achieved a phase transition in the nitrogen, it turning from liquid to solid. We computed the mass of the nitrogen evaporated required to reach its triple point temperature. We calculated the effective evacuation rate in the system, taking into account the conductivity of separate components. We determined the minimum vapour evacuation time required. We plotted system temperature and pressure as functions of time. The paper describes possible modernisation of the experimental installation, that is, introducing additional crystallisation centres and monitoring the liquid nitrogen mass using electronic scales


1990 ◽  
Vol 98 (1144) ◽  
pp. 1296-1301 ◽  
Author(s):  
Mitsuharu TABUCHI ◽  
Yasunari KANEKO ◽  
Hiromichi IWASAKI

2007 ◽  
Vol 334-335 ◽  
pp. 397-400 ◽  
Author(s):  
Sang Guk Kang ◽  
Myung Gon Kim ◽  
Sang Wuk Park ◽  
Chun Gon Kim ◽  
Cheol Won Kong

Nowadays, researches for replacing material systems for cryogenic propellant tanks by composites have been being performed for the purpose of light weight of a launch vehicle. In this paper, a type III propellant tank, which is composed of the composite developed for cryogenic use and an aluminum liner, was fabricated and tested considering actual operating environment, that is, cryogenic temperature and pressure. For this aim, liquid nitrogen (LN2) was injected into the fabricated tank and in turn, gaseous nitrogen (GN2) was used for pressurization. During this test procedure, strains and temperatures on the tank surface were measured. ESG (electric strain gage) and thermocouple were used for the measurement of strain and temperature, respectively. Delamination between hoop layer and helical one, was detected during the experiment. Finally, Tsai-Wu criterion for the tank and microscopy for the composite/aluminum ring specimen were carried out to investigate the reason why delamination had happened.


2000 ◽  
Vol 18 (1-6) ◽  
pp. 331-338 ◽  
Author(s):  
C. Pascal ◽  
R. M. Marin-Ayral ◽  
F. Martinez ◽  
J. C. Tedenac

Sign in / Sign up

Export Citation Format

Share Document