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MIL-A-8867C : AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
سازمان: NAVY - AS - Naval Air Systems Command
کلید واژه: Airplane tests , Arresting tests , Cabin pressure tests , Carrier-based airplanes , Catapult tests , Control system tests , Drop tests , Elevated temperature tests , Engine-mounted tests , Fatigue tests , Fuel tank leakage , Fuselage tests , Ground tests , Landing gear installation tests , Repeated load tests , Static tests , Strength tests , Tail group tests , Test measurements , Trainers , Vibration tests , Wing group tests
سال: 1987
زبان: English
قیمت: 290000 تومان
This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes. The types of testing include, but are not limited to:
a. Design development tests.
b. Pre-production component tests.
c. Static tests-complete airframe.
d. Fatigue tests-complete airframe.
e. Drop tests of structurally complete airframe.
f. Cabin pressure tests.
g. Leakage tests of integral fuel tanks.
h. Structural dynamic tests.
i. Proof tests for flight articles. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 53), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
MIL-A-8867C : AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
سازمان: NAVY - AS - Naval Air Systems Command
کلید واژه: Airplane tests , Arresting tests , Cabin pressure tests , Carrier-based airplanes , Catapult tests , Control system tests , Drop tests , Elevated temperature tests , Engine-mounted tests , Fatigue tests , Fuel tank leakage , Fuselage tests , Ground tests , Landing gear installation tests , Repeated load tests , Static tests , Strength tests , Tail group tests , Test measurements , Trainers , Vibration tests , Wing group tests
سال: 1987
زبان: English
قیمت: 290000 تومان
This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evaluation of fixed wing piloted airplanes. The types of testing include, but are not limited to:
a. Design development tests.
b. Pre-production component tests.
c. Static tests-complete airframe.
d. Fatigue tests-complete airframe.
e. Drop tests of structurally complete airframe.
f. Cabin pressure tests.
g. Leakage tests of integral fuel tanks.
h. Structural dynamic tests.
i. Proof tests for flight articles. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 53), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
