A review of nuclear propulsion rocket

سال انتشار: 1394
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 509

فایل این مقاله در 10 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

ICEASCONF01_268

تاریخ نمایه سازی: 9 مرداد 1395

چکیده مقاله:

This article offers a summary of past efforts in the development of Nuclear Thermal Propulsion systems for space transportation. First, the generic principle of thermal propulsion is outlined: a propellant is directly heated by a power source prior to being expanded which creates a thrusting force on the rocket.This enables deriving a motivation for the use of Nuclear Thermal Propulsion (NTP) relying on nuclear power sources.Then, a summary of major families of NTP systems is established on the basis of a literature survey.These families are distinguished by the nature of their power source, the most important being systems with radioisotope, fission, and fusion cores. Concepts proposing to harness the annihilation of matter and anti-matter are only touched briefly due to their limited maturity. For each family, an overview of physical fundamentals, technical concepts, and if available tested engines' propulsion parameters is given. I think the future of driving space. I think the future of nuclear thermal propulsion is good

کلیدواژه ها:

Nuclear Propulsion-fission propulsion- nuclear rocket

نویسندگان

Pooya Khoshkalamyan

Student at Isfahan University Of Technology, Chemical Engineering Department

Shaghayegh Arab

Ikco spare parts & after sales services,Isfahan,Dastgerd