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61. |
SWEPT FREQUENCY ULTRASONIC INSPECTION METHOD FOR LINER-PROPELLANT SEPARATIONS OF SOLID ROCKET MOTORS |
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Nondestructive Testing and Evaluation,
Volume 8-9,
Issue 1-6,
1992,
Page 1069-1083
MORIO SHIMIZU,
YUKIO FUKUSHIMA,
MICHIO TAKAHASHI,
KATSUYA ITOH,
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摘要:
This paper describes the swept frequency type of ultrasonic inspection method that is usable for inspecting liner-propellant separations of solid rocket motors and successful application of the method to the H-I upper-stage motors. Unfortunately, over the past quarter of a century, the liner-propellant separations have never been inspected practically with usual ultrasonic inspection methods. The special method has been developed at the National Aerospace Laboratory (NAL) since 1968, and the inspection technique is based on the one-dimensional quarter-wavelength resonance principle for the liner thickness under one free and the other fixed end-face boundary condition, which is considered the linear-propellant separation boundary condition of the linear. Since the motor cases have curved (spherical or cylindrical) surfaces, some curved contact surface probes were developed. This method was successfully applied to the apogee and third stage motor of the H-I rocket at the manufacturer and then at the launching site. This inspection has contributed to the successful launchings of the H-I rocket since the first launching in August 1987, and will be able to be applied to the solid rocket booster (SRB) of the H-II rocket in the near future.
ISSN:1058-9759
DOI:10.1080/10589759208952776
出版商:Taylor & Francis Group
年代:1992
数据来源: Taylor
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62. |
THE INTEGRITY EVALUATION OF THE WELD JOINT OF SPHERICAL ROCKET MOTOR CASE |
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Nondestructive Testing and Evaluation,
Volume 8-9,
Issue 1-6,
1992,
Page 1085-1097
Y. SHIRASUNA,
A. NOZUE,
T. OKUBO,
K. KURIBAYASHI,
R. HORIUCHI,
S. ISHIMOTO,
H. SATO,
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PDF (321KB)
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摘要:
The Institute of Space and Astronautical Science (ISAS) is undertaking the launching of spacecraft for space observations and interplanetary explorations. The spherical rocket motor case of satellite launchers was made of Ti-6A1-4V alloy, however, to reduce the weight and fabrication cost, the material of the case was changed to Ti-15V-3Cr-3Sn-3AI alloy because of its good cold formability and the high strength. However, it was found that the hardness of weld joint was higher than that of base metal and the fracture toughness was lower when heat treated by a conventional aging process.
ISSN:1058-9759
DOI:10.1080/10589759208952777
出版商:Taylor & Francis Group
年代:1992
数据来源: Taylor
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