Miniscale ballistic motor testing method for rocket propellants
Patent 5419116 Issued on May 30, 1995. Estimated Expiration Date: 
March 15, 2014. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.
March 15, 2014. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.Patent References 3015231 Solid propellant measurement system Method for burning rate characterization of solid propellants Patent #: 4554823 InventorsApplicationNo. 213283 filed on 03/15/1994US Classes:60/204, Method of operation60/253, Solid propellant73/116MOTOR AND ENGINE TESTINGExaminersPrimary: Bertsch, Richard A.Assistant: Wicker, William Attorney, Agent or FirmInternational ClassG01L 003/26AbstractA method for using a miniscale ballistic test motor for determining burn es over an operating pressure range allows the testing of a small propellant sample. The small propellant sample allows performance of an abbreviated procedure for each test of the propellant sample involving loading of a small scale test motor with the sample, conditioning the test motor and sample therein, firing the propellant sample and recording data. | |
