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Archive | 2018

Experiment STAbility of liquid COlumns (STACO) on the Advanced Fluid Physics Module (FPM) aboard Spacelab-D2

Isidoro Martínez Herranz; José Manuel Perales Perales; José Meseguer Ruiz; Ulrich Walter

During the second German Mission of Spacelab (1993, Spacelab D-2) an experiment on the mechanical stability of liquid columns was performed. A liquid column is a liquid mass held between to solid (circular) supports. A 30 mm in diameter and 90 mm long liquid drop was stablished in the Advanced Fluid Physics Module (AFPM) and was subjected to different mechanical stimuli (rotation of the supports, oscillation of one of the supports, change in volume and in length) to check whether the resulting drop was stable or not. Results were obtained in terms of images and recorded in a video sequence. Telemetry of the different stimuli and parameter values was also recorded. Objetive: The aim of this experiment was to measure the outer shape deformation of long liquid bridges near their stability limit under microgravity, caused by g-jitters and by some controlled mechanical disturbances (change of geometry, change of volume, rotation and vibration). The liquid used was a silicone-oil 10 times more viscous than water (5 times for the last run). The working length of the liquid column was 85 mm. The two solid supports are made of aluminium, of 30 mm in diameter, with a sharp cutback (30 deg. edge) to prevent liquid spreading over the edges. This choice of geometry allows a direct comparison with other TEXUS experiments where two discs of 30 mm in diameter and 86 mm apart were used to hold a cylindrical liquid column (35 mm discs were used in SL-D1 and 40 mm discs on SL-1). A top priority was to verify the results of a previous experiment performed on SL-D1, and because an equivalent Bond number Bo=0.007 was deduced from this experiment and there was no reason to expect a different behaviour, it was planned, in a second run to make use of unequal discs of 30 mm and 28 mm in a second run to precisely counterbalance the expected deformation and better quantify this effect. Procedures: The actual procedures executed were: -- Run 1: background sensing, disc oscillation at 0.40 Hz, 0.41 Hz, 0.42 Hz and again 0.42 Hz. -- Run 2: background sensing and disc separation until breakage of the column. -- Run 3: background sensing. Results: An example of free oscillations of a liquid column (diameter 30 mm, length 85 mm, volume 60 cc), due to g-jitter, is shown in Video1, recorded during the background sensing phase of Run 2. Video2 shows the breakage of the same column caused by disc separation at constant volume. This experiment enabled to accurately measure the response of the 85 mm-long cylindrical liquid column to a forced axial vibration of one of the supporting discs, and found that it is in very good agreement with theory, and complements other measurements performed in the same flight but with shorter columns by D. Langbein. An achievement is the high accuracy reached in automatic image analysis, of the order of 30 microns in object size (0.1 pixels in the 512*512 image), which represents a great improvement in comparison to the manually digitised hard-prints of previous flights. The more puzzling question left after the experiment is the lack of reproducibility of the steady averaged deformation measurement, perhaps because it is not a characteristic of the configuration and may be dependent on details of hardware (e.g. materials used, rounding of wetted corners) that escape control of the experimenter and are different for each campaign. As usual, more experiments are needed to elucidate the unexpected results of this one, but a clear progress in the overall experiment planning is evident.


Material science in space : proceedings | Third European Symposium on Material Science in Space | 24-27 April | Grenoble | 1979

Floating zone stability

Ignacio Da Riva de la Cavada; Isidoro Martínez Herranz


Spacecraft thermal and environmental control systems | International Symposium on Spacecraft Thermal and Environmental Control Systems | 10-12 Oct 1978 | Munich | 1978

Spacecraft thermal control design data

Ignacio Da Riva de la Cavada; José Meseguer Ruiz; Isidoro Martínez Herranz; C Stroom


ESA Journal, ISSN 0379-2285, 1985, Vol. 9 | 1985

Long liquid bridges aboard sounding rockets

Isidoro Martínez Herranz; Angel Pedro Sanz Andres


ESA, Proceedings of the 8th European Symposium on Materials and Fluid Sciences in Microgravity | 8th European Symposium on Materials and Fluid Sciences in Microgravity | 12/04/1992-16/041992 | Bruselas, Belgica | 1992

Effects of Axial and Centrifugal Forces on the Stability of Liquid Bridges

Isidoro Martínez Herranz; José Manuel Perales Perales; M. Gomez


ESA Journal, ISSN 0915-3616, 1988, Vol. 12 | 1988

Freezing of a Long Liquid Column on the Texus-18 Sounding Rocket Flight

Isidoro Martínez Herranz; Angel Pedro Sanz Andres; José Manuel Perales Perales; José Meseguer Ruiz


Space Research#R##N#Proceedings of the Open Meetings of the Working Groups on Physical Sciences of the Twentieth Plenary Meeting of COSPAR, Tel Aviv, Israel, 7–18 June 1977 | 1978

FLOATING ZONE-EQUILIBRIUM SHAPES AND STABILITY CRITERIA

Isidoro Martínez Herranz


Mechanical behaviour of liquid bridges in microgravity | En: Physics of Fluids in Microgravity | pag. 21-45 | Taylor & Francis | 2002-01 | 2002

Mechanical behaviour of liquid bridges in microgravity

Isidoro Martínez Herranz; José Manuel Perales Perales


Proceedings of the 38th COSPAR Scientific Assembly 2010 | 38th COSPAR Scientific Assembly 2010 | 18/07/2010 - 25/07/2010 | Bremen, Alemania | 2010

Experimental analysis of the vibration of a liquid bridge under microgravity conditions.

José Manuel Perales Perales; Isidoro Martínez Herranz


Current Topics in Crystal Growth Research, ISSN 0167-6105, 1999, Vol. 5 | 1999

Hydrostatic instabilities in floating zone cristal growth process

José Meseguer Ruiz; José Manuel Perales Perales; Isidoro Martínez Herranz

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José Meseguer Ruiz

Technical University of Madrid

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