[go: up one dir, main page]

Rochford, 1999 - Google Patents

Temperature sensitivity measurements of solid rocket propellants

Rochford, 1999

Document ID
12449815763615707253
Author
Rochford E
Publication year

External Links

Snippet

A method of measuring the burning rate and temperature sensitivity of burning rate of solid rocket propellants was investigated. The investigation was accomplished through experimental laboratory work. Selected propellants were studied using an ultrasonic pulse …
Continue reading at search.proquest.com (other versions)

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Similar Documents

Publication Publication Date Title
Vernacchia et al. Low-thrust solid rocket motors for small, fast aircraft propulsion: Design and development
US6342186B1 (en) Ceramic liner for closed bomb applications
Chiaverini Regression rate and pyrolysis behavior of HTPB-based solid fuels in a hybrid rocket motor
Fry Solid propellant subscale burning rate analysis methods for US and selected NATO facilities
Rochford Temperature sensitivity measurements of solid rocket propellants
Fry Solid propellant test motor scaling
Bernecker The deflagration-to-detonation transition process for high-energy propellants-a review
Evans et al. Solid-fuel ramjet regression rate measurements using x-ray radiography and ultrasonic transducers
Jeenu et al. Industrial adaptation of ultrasonic technique of propellant burning rate measurement using specimens
Evans et al. Instantaneous regression rate determination of a cylindrical x-ray transparent hybrid rocket motor
Sapozhnikov et al. Investigation of the ablative properties of an EPDM\kevlar insulator in a solid rocket motor
Rodenberger et al. Feasibility of Obtaining Hypervelocity Acceleration Using Propellant Lined Launch Tubes
Saucedo-Zárate et al. Captive-fired experiment of a solid rocket motor
Borg Additively manufactured granular and binder metamaterial’s response to shock
DELUCA CHAPTER SEVEN BURNING RATE ISSUES IN SOLID ROCKET PROPULSION: PART I. FUNDAMENTALS
Mcknight Advanced hybrid rocket motor propulsion unit for cubesats
Roberts Shock tube ignition and combustion of aluminum/magnesium alloy particles in oxygen at high pressure
Carter et al. Development and Demonstration of a N2O4/N2H4 Injector
van den Wijngaart A study on effects of geometry on internal ballistics of multiple BATES grain Solid Rocket Motors
Beckman et al. Ballistic anomaly trends in subscale solid rocket motors
Gerards High pressure ballistic evaluation motor: The development and characterization of the Army Ten-Pound Charge (ATPC) motor
Baker Drop-weight impact initiation of ammonium perchlorate composite solid rocket propellants
Kuo et al. Study of Dynamic Behavior and Hazards of VHBR, LOVA, And PSS Propellants under Rapid Ignition And Combustion Conditions by Real-Time X-Ray Radiography
Begeal Through bulkhead initiator studies
Jacobs et al. An Experimental Study of the Pressure Distribution in Burning Flaws in Solid Propellant Grains