دورية أكاديمية
HIGH- AND LOW-TEMPERATURE TESTS OF THE AEROJET UTILITY VAN
| العنوان: | HIGH- AND LOW-TEMPERATURE TESTS OF THE AEROJET UTILITY VAN |
|---|---|
| المؤلفون: | Sohl, J. D. |
| المساهمون: | AEROJET-GENERAL CORP SACRAMENTO CA |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1962 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Surface Transportation and Equipment, VEHICLES, HIGH TEMPERATURE, TEST METHODS, INSTRUMENTATION, TRAILERS, TEMPERATURE CONTROL, PHOTOGRAPHS, SURFACE TO SURFACE MISSILES, GROUND SUPPORT EQUIPMENT, ROCKET ENGINES, SOLID PROPELLANT ROCKET ENGINES, TEMPERATURE, CALIBRATION, CARRIERS(VEHICLES), MINUTEMAN MISSILES |
| الوصف: | the utility van successfully completed highand low-temperature tests to verify its acceptability as a transport vehicle for secondstage Minuteman operational motors. A Minuteman motor cast with propellant simulant was used in the tests. While the exterior of the van was subjected to high and low temperatures, ranging from 140 to -35 F, the surface of the motor was maintained within the specified temperature range of 80+/-20 F. |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| العلاقة: | http://www.dtic.mil/docs/citations/AD0296254Test |
| الإتاحة: | http://www.dtic.mil/docs/citations/AD0296254Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0296254Test |
| حقوق: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.BE9F1058 |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |