دورية أكاديمية
Solid-Propellant-Powered Maneuvering System for Spacecraft.
العنوان: | Solid-Propellant-Powered Maneuvering System for Spacecraft. |
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المؤلفون: | Goddard, Charles W, Lucas, John T, Galvan, Paul A |
المساهمون: | DEPARTMENT OF THE NAVY WASHINGTON DC |
المصدر: | DTIC AND NTIS |
سنة النشر: | 1991 |
المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
مصطلحات موضوعية: | Ammunition and Explosives, GAS GENERATING SYSTEMS, MANIFOLDS(ENGINES), NOZZLE CLUSTERS, PROPELLANT BURN OUT, SEQUENCES, SPACECRAFT, VALVES, Patents, PAT-CL-244-169, Solid propellants, Maneuverability |
الوصف: | An improvement to a variable-pressure solid-propellant-powered maneuvering system for spacecraft, enabling the system to operate for longer than one propellant burn time. At least two solid propellant gas generators are connected via a manifold to a plurality of nozzle valve clusters; at least one of the gas generators is connected to the manifold via a sequence valve which isolates that generator from the manifold until such time as it is desired to put that generator into operation. ; Supersedes PAT-APPL-660 361-91. |
نوع الوثيقة: | text |
وصف الملف: | text/html |
اللغة: | English |
العلاقة: | http://www.dtic.mil/docs/citations/ADD015245Test |
الإتاحة: | http://www.dtic.mil/docs/citations/ADD015245Test http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADD015245Test |
حقوق: | Availability: This Government-owned invention available for U.S. licensing and, possibly, for foreign licensing. Copy of patent available Commissioner of Patents, Washington, DC 20231. $1.50 |
رقم الانضمام: | edsbas.A7A9A093 |
قاعدة البيانات: | BASE |
الوصف غير متاح. |