SEDS Tether M/OD Damage Analyses PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download SEDS Tether M/OD Damage Analyses PDF full book. Access full book title SEDS Tether M/OD Damage Analyses by K. B. Hayashida. Download full books in PDF and EPUB format.
Author: K. B. Hayashida
Publisher:
ISBN:
Category : Microspacecraft
Languages : en
Pages : 36
Get Book Here
Book Description
Author: K. B. Hayashida
Publisher:
ISBN:
Category : Microspacecraft
Languages : en
Pages : 36
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1250
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
Get Book Here
Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722761547
Category :
Languages : en
Pages : 32
Get Book Here
Book Description
The Small Expendable Deployer System (SEDS) was designed to deploy an endmass at the end of a 20-km-long tether which acts as an upper stage rocket, and the threats from the meteoroid and orbital debris (M/OD) particle environments on SEDS components are important issues for the safety and success of any SEDS mission. However, the possibility of severing the tether due to M/OD particle impacts is an even more serious concern, since the SEDS tether has a relatively large exposed area to the M/OD environments although its diameter is quite small. The threats from the M/OD environments became a very important issue for the third SEDS mission, since the project office proposed using the shuttle orbiter as a launch platform instead of the second stage of a Delta II expendable rocket, which was used for the first two SEDS missions. A series of hyper-velocity impact tests were performed at the Johnson Space Center and Arnold Engineering Development Center to help determine the critical particle sizes required to sever the tether. The computer hydrodynamic code or hydrocode called CTH, developed by the Sandia National Laboratories, was also used to simulate the damage on the SEDS tether caused by both the orbital debris and test particle impacts. The CTH hydrocode simulation results provided the much needed information to help determine the critical particle sizes required to sever the tether. The M/OD particle sizes required to sever the tether were estimated to be less than 0.1 cm in diameter from these studies, and these size particles are more abundant in low-Earth orbit than larger size particles. Finally, the authors performed the M/OD damage analyses for the three SEDS missions; i.e., SEDS-1, -2, and -3 missions, by using the information obtained from the hypervelocity impact test and hydrocode simulations results. Hayashida, K. B. and Robinson, J. H. and Hill, S. A. Marshall Space Flight Center ...
Author: Evgeniĭ Mikhaĭlovich Levin
Publisher: Univelt Incorporated
ISBN: 0877035385
Category : Science
Languages : en
Pages : 463
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 602
Get Book Here
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Luciano Guerriero
Publisher: Compositori
ISBN:
Category : Science
Languages : en
Pages : 696
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Tethered satellites
Languages : en
Pages : 468
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 290
Get Book Here
Book Description
