دورية أكاديمية

Solid-Propellant-Powered Maneuvering System for Spacecraft.

التفاصيل البيبلوغرافية
العنوان: Solid-Propellant-Powered Maneuvering System for Spacecraft.
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