東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Developing hybrid near-space technol...

Badders, Brian David.

FindBook

Google Book

Amazon

博客來

Developing hybrid near-space technologies for affordable access to suborbital space.

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Developing hybrid near-space technologies for affordable access to suborbital space./
作者:	Badders, Brian David.
面頁冊數:	155 p.
附註:	Source: Masters Abstracts International, Volume: 52-05.
Contained By:	Masters Abstracts International52-05(E).
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1552173
ISBN:	9781303713392

Developing hybrid near-space technologies for affordable access to suborbital space.
Badders, Brian David.

Developing hybrid near-space technologies for affordable access to suborbital space. - 155 p.

Source: Masters Abstracts International, Volume: 52-05.

Thesis (M.S.)--The University of North Dakota, 2013.

High power rockets and high altitude balloons are two near-space technologies that could be combined in order to provide access to the mesosphere and, eventually, suborbital space. This "rockoon" technology has been used by several large budget space programs before being abandoned in favor of even more expensive, albeit more accurate, ground launch systems. With the increased development of nano-satellites and atmospheric sensors, combined with rising interest in global atmospheric data, there is an increase in desire for affordable access to extreme altitudes that does not necessarily require the precision of ground launches.

ISBN: 9781303713392Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Developing hybrid near-space technologies for affordable access to suborbital space.
LDR:03582nam a2200313 4500 001 1963174
005 20140929140117.5
008 150210s2013 ||||||||||||||||| ||eng d
020 $a 9781303713392
035 $a (MiAaPQ)AAI1552173
035 $a AAI1552173
040 $a MiAaPQ $c MiAaPQ
100 1 $a Badders, Brian David. $3 2099360
245 1 0 $a Developing hybrid near-space technologies for affordable access to suborbital space.
300 $a 155 p.
500 $a Source: Masters Abstracts International, Volume: 52-05.
500 $a Adviser: Ronald A. Fevig.
502 $a Thesis (M.S.)--The University of North Dakota, 2013.
520 $a High power rockets and high altitude balloons are two near-space technologies that could be combined in order to provide access to the mesosphere and, eventually, suborbital space. This "rockoon" technology has been used by several large budget space programs before being abandoned in favor of even more expensive, albeit more accurate, ground launch systems. With the increased development of nano-satellites and atmospheric sensors, combined with rising interest in global atmospheric data, there is an increase in desire for affordable access to extreme altitudes that does not necessarily require the precision of ground launches.
520 $a Development of hybrid near-space technologies for access to over 200k ft. on a small budget brings many challenges within engineering, systems integration, cost analysis, market analysis, and business planning. This research includes the design and simulation testing of all the systems needed for a safe and reusable launch system, the cost analysis for initial production, the development of a business plan, and the development of a marketing plan. This project has both engineering and scientific significance in that it can prove the space readiness of new technologies, raise their technology readiness levels (TRLs), expedite the development process, and also provide new data to the scientific community. It also has the ability to stimulate university involvement in the aerospace industry and help to inspire the next generation of workers in the space sector.
520 $a Previous development of high altitude balloon/high power rocket hybrid systems have been undertaken by government funded military programs or large aerospace corporations with varying degrees of success. However, there has yet to be a successful flight with this type of system which provides access to the upper mesosphere in a university setting. This project will aim to design and analyze a viable system while testing the engineering process under challenging budgetary constraints. The technical, engineering, and systems integration challenges that will be investigated are rocket design, launch platform design, communications, ignition systems, recovery systems, and stabilization methods. This will be done using rocket performance simulation software, computer-aided design software, and computational fluid dynamic analysis software.
520 $a The business planning is also an important part of this research. Through detailed market analysis, the needs for the proposed product/services being developed will be assessed. Through the combination of detailed cost analysis and the market needs, the economic viability of this launch system will be determined.
590 $a School code: 0156.
650 4 $a Engineering, Aerospace. $3 1018395
650 4 $a Business Administration, Entrepreneurship. $3 1026793
690 $a 0538
690 $a 0429
710 2 $a The University of North Dakota. $b Space Studies. $3 2099361
773 0 $t Masters Abstracts International $g 52-05(E).
790 $a 0156
791 $a M.S.
792 $a 2013
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1552173