PSP Bibliography





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Found 3 entries in the Bibliography.


Showing entries from 1 through 3


2015

Glass Surface Spall Size Resulting From Interplanetary Dust Impacts

The size of relatively large dynamic conchoidal fractures, i.e., surface spalls, immediately adjacent to and around interplanetary dust (IDP) hypervelocity impact (HVI) craters or pits in glass substrates is relevant to spacecraft solar cell and science instrument lens performance metrics, as well as glass pane design and safety in manned missions. This paper presents an analysis of the diameter of surface spalls in glass for the Solar Probe Plus (SPP) spacecraft, whose solar arrays and instruments must survive a 7-year miss ...

Iyer, Kaushik; Mehoke, Douglas; Chadegani, Alireza; Batra, Romesh;

Published by:       Published on:

YEAR: 2015     DOI: 10.1109/AERO.2015.7119067

Parker Data Used

2013

Hypervelocity Impact Response of Ti-6Al-4V and Commercially Pure Titanium

Titanium alloy, Ti-6Al-4V, and commercially pure (CP) Titanium will be used to protect the Solar Probe Plus (SPP) spacecraft against hypervelocity impacts by solar dust particles. The results of six hypervelocity impact (HVI) tests performed on Ti-6Al-4V and CP monolithic samples (3 each) arc evaluated in terms of cratering and spall damage, and compared with crater depth and spall initiation predictions using the Ballistic Limit Equation (BLE) for Titanium shields developed at NASA Johnson Space Center and hydrocode computa ...

Iyer, Kaushik; Poormon, Kevin; Deacon, Ryan; Mehoke, Douglas; Swaminathan, P.; Brown, Robert;

Published by:       Published on:

YEAR: 2013     DOI: 10.1016/j.proeng.2013.05.016

Parker Data Used

2012

Use of Hydrocode Modeling to Develop Advanced MMOD Shielding Designs

A multi-physics computations-based methodology for space debris hypervelocity impact (HVI) damage mitigation is presented. Specifically, improved debris mitigation through development of innovative, lightweight structural designs is described. The methodology has been applied to the design of the Solar Probe Plus (SPP) spacecraft to mitigate extreme solar microdust hypervelocity impacts (50-300 km/s) by the Johns Hopkins University Applied Physics Laboratory (JHU/APL). The methodology combines hydrocode computations of the c ...

Iyer, Kaushik; Mehoke, Douglas; Brown, Robert; Swaminathan, P.; Carrasco, Cesar; Batra, Romesh;

Published by:       Published on:

YEAR: 2012     DOI: 10.1109/AERO.2012.6187075

Parker Data Used



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