Electronic Resource

AFRPL Connector Tests

التفاصيل البيبلوغرافية
العنوان: AFRPL Connector Tests
المؤلفون: AIR FORCE ROCKET PROPULSION LAB EDWARDSAFB CA, Graves, George N.
المصدر: DTIC AND NTIS
بيانات النشر: 1969-05
نوع الوثيقة: Electronic Resource
مستخلص: A family of threaded fittings was developed which would withstand the stringent operating conditions imposed on a fluid line connector by a liquid rocket. Qualification and verification testing of this connector family was conducted and the results evaluated in a program of the AFRPL. The tests include repeated assembly, thermal gradient, stress-reversal bending, and pressure impulse. Connectors which were tested and qualified were fabricated from type 347 CRES in the 1/4, 3/8, and 1/2 inch O.D. sizes. The complete family of connectors includes a 3/4 and 1 inch O.D. size. A complete test system was developed for qualifying and testing any threaded connector.
مصطلحات الفهرس: Couplers, Fasteners, and Joints, Rocket Engines, LIQUID PROPELLANT ROCKET ENGINES, ENGINE FUEL SYSTEMS COMPONENTS, SELF SEALING COUPLINGS, PERFORMANCE(ENGINEERING), LEAKAGE(FLUID), STAINLESS STEEL, TEST EQUIPMENT, BENDING, RUPTURE, RELIABILITY, THERMAL EXPANSION, STANDARDS, ASSEMBLY, FUEL SEALS, DISCONNECT FITTINGS, METAL SEALS., AFRPL CONNECTORS, BOBBIN SEALS, DIMENSIONS, EVALUATION, IMPULSE PRESSURE, Text
URL: https://apps.dtic.mil/docs/citations/AD0857538
الاتاحة: Open access content. Open access content
APPROVED FOR PUBLIC RELEASE
ملاحظة: text/html
English
Other Numbers: DTICE AD0857538
831783831
المصدر المساهم: From OAIster®, provided by the OCLC Cooperative.
رقم الانضمام: edsoai.ocn831783831
قاعدة البيانات: OAIster