A fluid ejection system for ballistic range testing

1968 ◽  
Author(s):  
A. GIESECKE ◽  
A. HAMMITT
Keyword(s):  
Ballistic Range ◽  
Range Testing

Global Pressure and Temperature Measurements of Ballistic-Range Testing by PSP and TSP Techniques

2014 ◽  
Author(s):  
Hirotaka Sakaue ◽  
Yoshimi Iijima ◽  
Yuki Yamada ◽  
Takeshi Miyazaki ◽  
Masato Ishii
Keyword(s):  
Temperature Measurements ◽  
Ballistic Range ◽  
Range Testing ◽  
Global Pressure

Development of an RF induction plasma generator for ballistic range testing

2000 ◽  
Author(s):  
Heard Lowry ◽  
Les Crosswy ◽  
Joel Mansfield ◽  
Dennis Keefer ◽  
Monty Smith ◽  
...  
Keyword(s):  
Plasma Generator ◽  
Induction Plasma ◽  
Ballistic Range ◽  
Range Testing ◽  
Rf Induction Plasma

scholarly journals Ballistic Range Testing Data Analysis of Tianwen-1 Mars Entry Capsule

2021 ◽  
Vol 2021 ◽  
pp. 1-6
Author(s):  
Haogong Wei ◽  
Xin Li ◽  
Jie Huang ◽  
Qi Li ◽  
Wei Rao
Keyword(s):  
Dynamic Instability ◽  
Linear Regression Method ◽  
Ballistic Range ◽  
Mass Properties ◽  
Testing Data ◽  
Supersonic Regime ◽  
Range Testing ◽  
Mach Numbers ◽  
Scaled Models ◽  
Range Test

A typical blunt body such as Tianwen-1 Mars entry capsule suffers dynamic instability in supersonic regime. To investigate the unstable Mach range of flight and to confirm the design of aerodynamic shape and mass properties, a ballistic range test was carried out aiming at capturing supersonic dynamic characteristics of Tianwen-1. Aerodynamic coefficients of free-flight scaled models were derived by modified linear regression method based on position and attitude data, while the dynamic coefficients were established under the assumption of small angle linearization. The static moment coefficients and dynamic derivatives were identified thereafter. Results show that models in untrimmed configuration are dynamically unstable at certain Mach numbers, whereas models in trimmed configuration are dynamically stable at other Mach numbers tested. Both trimmed and untrimmed configurations are statically stable in all testing cases.

Ram accelerator ballistic range concept for softly accelerating hypersonic free-flying models

1994 ◽  
Vol 31 (6) ◽  
pp. 1310-1316 ◽  
Author(s):  
K. Wieland Naumann ◽  
Adam P. Bruckner
Keyword(s):  
Ram Accelerator ◽  
Ballistic Range

Reducing ballistic range data for the projectile's drag coefficient

AIAA Journal ◽  
1970 ◽  
Vol 8 (12) ◽  
pp. 2297-2299
Author(s):  
C. T. CROWE ◽  
R. CARLSON
Keyword(s):  
Drag Coefficient ◽  
Range Data ◽  
Ballistic Range

scholarly journals Review of background oriented schlieren and development for ballistic range applications

2013 ◽  
Vol 45 ◽  
pp. 01034 ◽  
Author(s):  
Ardian B. Gojani ◽  
Burim Kamishi ◽  
Shigeru Obayashi
Keyword(s):  
Ballistic Range ◽  
Background Oriented Schlieren
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