Suman Chakrabarti
Marshall Space Flight Center
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Featured researches published by Suman Chakrabarti.
ieee aerospace conference | 2013
Chantrice Moss; Suman Chakrabarti; David W. Scott
A United States Government Accountability Office (GAO) review of twelve NASA programs found widespread parts quality problems contributing to significant cost overruns, schedule delays, and reduced system reliability. Direct part marking with Data Matrix symbols could significantly improve the quality of inventory control and parts lifecycle management. This paper examines the feasibility of using direct part marking technologies for use in future NASA programs. A structural analysis is based on marked material type, operational environment (e.g., ground, suborbital, Low Earth Orbit), durability of marks, ease of operation, reliability, and affordability. A cost-benefits analysis considers marking technology (label printing, data plates, and direct part marking) and marking types (two-dimensional machine-readable, human-readable). Previous NASA parts marking efforts and historical cost data are accounted for, including in-house vs. outsourced marking. Some marking methods are still under development. While this paper focuses on NASA programs, results may be applicable to a variety of industrial environments.
SPACE TECHNOLOGY AND APPLICATIONS INT.FORUM-STAIF 2003: Conf.on Thermophysics in Microgravity; Commercial/Civil Next Generation Space Transportation; Human Space Exploration; Symps.on Space Nuclear Power and Propulsion (20th); Space Colonization (1st) | 2003
James Martin; Raymond Lewis; Suman Chakrabarti; William H. Sims; J. Boise Pearson; Wallace E. Fant
To take the first step towards using the energy produced from the matter‐antimatter annihilation for propulsion applications, the NASA Marshall Space Flight Center (MSFC) Propulsion Research Center (PRC) has initiated a research activity examining the storage of low energy antiprotons. The High Performance Antiproton Trap (HiPAT) is an electromagnetic system (Penning‐Malmberg design) consisting of a 4 Tesla superconductor, a high voltage electrode confinement system, and an ultra high vacuum test section. It has been designed with an ultimate goal of maintaining 1012 charged particles with a half‐life of 18 days. Currently, this system is being evaluated experimentally using normal matter ions that are cheap to produce, relatively easy to handle, and provide a good indication of overall trap behavior (with the exception of assessing annihilation losses). The ions are produced via a positive hydrogen ion source and transported to HiPAT in a beam line equipped with electrostatic optics. The optics serve to ...
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM- STAIF 2002 | 2002
James Martin; Raymond Lewis; Suman Chakrabarti; Boise Pearson
The matter antimatter reaction represents the densest form of energy storage/release known to modern physics: as such it offers one of the most compact sources of power for future deep space exploration. To take the first steps along this path, the NASA-MSFC is developing a storage system referred to as the High Performance Antiproton Trap (HiPAT) with a goal of maintaining 1012 particles for up to 18 days. Experiments have been performed with this hardware using normal matter (positive hydrogen ions) to assess the device’s ability to hold charged particles. These ions are currently created using an electron gun method to ionize background gas; however, this technique is limited by the quantity that can be captured. To circumvent this issue, an ion source is currently being commissioned which will greatly increase the number of ions captured and more closely simulate actual operations expected at an antiproton production facility. Ions have been produced, stored for various time intervals, and then extrac...
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 2000 | 2000
Mike Houts; Joe Bonometti; Jeff Morton; Ivana Hrbud; Leo Bitteker; Melissa Van Dyke; Tom Godfroy; Kevin Pedersen; Chris Dobson; Bruce Patton; James Martin; Suman Chakrabarti
Fission technology can enable rapid, affordable access to any point in the solar system. Potential fission-based transportation options include bimodal nuclear thermal rockets, high specific energy propulsion systems, and pulsed fission propulsion systems. In-space propellant re-supply enhances the effective performance of all systems, but requires significant infrastructure development. Safe, timely, affordable utilization of first-generation space fission propulsion systems will enable the development of more advanced systems. First generation space systems will build on over 45 years of US and international space fission system technology development to minimize cost.
Archive | 2004
James Martin; Raymond A. Lewis; William H. Sims; Suman Chakrabarti; Boise Pearson; Wallace E. Fant
Archive | 2003
James Martin; Raymond A. Lewis; J. Boise Pearson; W. Herb Sims; Suman Chakrabarti; Wallace E. Fant; Stan McDonald
Archive | 2003
James Martin; Raymond A. Lewis; J. Boise Pearson; W. Herb Sims; Suman Chakrabarti; Wallace E. Fant; Stan McDonald
Archive | 2002
Raymond Lewis; James Martin; Suman Chakrabarti; Stephen L. Rodgers
Archive | 2002
J. Boise Pearson; James Martin; William H. Sims; Suman Chakrabarti; Raymond A. Lewis; Stephen L. Rodgers
Archive | 2002
James Martin; Raymond A. Lewis; J. Boise Pearson; W. Herb Sims; Suman Chakrabarti; Wallace E. Fant; Stan McDonald