scholarly journals Microgravity Experiment System using Free-fall Capsule from a High Altitude Balloon (Result of the 2nd Test Flight)

Author(s):  
Takehiko ISHIKAWA ◽  
Tatsuaki HASHIMOTO ◽  
Shujiro SAWAI ◽  
Yoshitaka SAITO ◽  
Yuko INATOMI ◽  
...  
2015 ◽  
Vol 63 (6) ◽  
pp. 257-264
Author(s):  
Yusuke MARU ◽  
Takehiko ISHIKAWA ◽  
Nobutaka BANDO ◽  
Shujiro SAWAI ◽  
Shigehito SHIMIZU ◽  
...  

1996 ◽  
Vol 64 (10) ◽  
pp. 1242-1246 ◽  
Author(s):  
Pirooz Mohazzabi ◽  
James H. Shea
Keyword(s):  

2010 ◽  
Vol 78 (6) ◽  
pp. 616-619 ◽  
Author(s):  
Jan Benacka
Keyword(s):  

2012 ◽  
Vol 5 (11) ◽  
pp. 2625-2633 ◽  
Author(s):  
T. J. Garrett ◽  
C. Fallgatter ◽  
K. Shkurko ◽  
D. Howlett

Abstract. We describe here a new instrument for imaging hydrometeors in free fall. The Multi-Angle Snowflake Camera (MASC) captures high-resolution photographs of hydrometeors from three angles while simultaneously measuring their fall speed. Based on the stereoscopic photographs captured over the two months of continuous measurements obtained at a high altitude location within the Wasatch Front in Utah, we derive statistics for fall speed, hydrometeor size, shape, orientation and aspect ratio. From a selection of the photographed hydrometeors, an illustration is provided for how the instrument might be used for making improved microwave scattering calculations. Complex, aggregated snowflake shapes appear to be more strongly forward scattering, at the expense of reduced back-scatter, than heavily rimed graupel particles of similar size.


2011 ◽  
Vol 89 (10) ◽  
pp. 1003-1008 ◽  
Author(s):  
Jan Benacka

In this study, the formulas for projectile velocity components and coordinates in a vacuum were derived with the altitude decrease in gravitational acceleration factored in. A model of cannon shell motion in the air is presented that accounts for the altitude dependence of gravitational acceleration, air density, the speed of sound up to an altitude of 84 km, and the speed dependence of the drag coefficient at trans- and supersonic speeds. The drag coefficient function is obtained by fitting to experimental data taken for the US M101 155 mm shell. The model gives flight parameters that agree with the published ones. The motion of the Paris Gun projectile is then modeled. The model shows that a range of 120 km is possible if the projectile mass is about 150 kg. A flat Earth approximation was used in the computations. Changing the launch angle to 90°, super high-altitude vertical ascent and free fall are modeled.


1985 ◽  
Vol 5 (1) ◽  
pp. 83-86 ◽  
Author(s):  
M. Namiki ◽  
S. Ohta ◽  
T. Yamagami ◽  
Y. Koma ◽  
H. Akiyama ◽  
...  

2013 ◽  
Vol 84 (9) ◽  
pp. 961-970 ◽  
Author(s):  
James M. Pattarini ◽  
Rebecca S. Blue ◽  
Luke T. Aikins ◽  
Jennifer Law ◽  
Andrew D. Walshe ◽  
...  

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