Electronic Resource
Fabrication and Test of an Advanced Expander Combustor
| العنوان: | Fabrication and Test of an Advanced Expander Combustor |
|---|---|
| المؤلفون: | PRATT AND WHITNEY WEST PALM BEACH FL LIQUID SPACE PROPULSION, Jennings, T., Fentress, S., Lyda, R. |
| المصدر: | DTIC AND NTIS |
| بيانات النشر: | 2000-06 |
| نوع الوثيقة: | Electronic Resource |
| مستخلص: | This paper discusses fabrication and test of an advanced expander combustion chamber for a 50.000 pound (222.4 kN) thrust Upper Stage Expander Cycle Engine. The chamber is being developed by Pratt & Whitney Liquid Space Propulsion under contract for the United States Air Force Research Laboratory (AFRL) to support the Integrated High Payoff Rocket Propulsion Technology (IHPRPT) initiative. The Advanced Expander Combustor is designed to provide increased heat pick-up to the coolant and improved system thrust to weight, increased specific impulse, and increased reliability. Pres. at AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit, (36th). Held in Huntsville, AL, 17-19 Jul 2000. AIAA paper 2000-3776. |
| مصطلحات الفهرس: | Combustion and Ignition, Liquid Propellant Rocket Engines, COMBUSTION CHAMBERS, LIQUID PROPELLANT ROCKET ENGINES, COMBUSTORS, ROCKET PROPULSION, THRUST CHAMBERS., PROCEEDINGS, EXPANDER CYCLE ENGINES, WUAFRL101100KQ, Text |
| URL: | |
| الاتاحة: | Open access content. Open access content APPROVED FOR PUBLIC RELEASE |
| ملاحظة: | text/html English |
| Other Numbers: | DTICE ADA408495 834240954 |
| المصدر المساهم: | From OAIster®, provided by the OCLC Cooperative. |
| رقم الانضمام: | edsoai.ocn834240954 |
| قاعدة البيانات: | OAIster |
| الوصف غير متاح. |