Anita Sengupta

发表

Comparison of Subscale versus Full Scale Wind Tunnel Tests of MSL Disk Gap Band Parachutes

Mike Kandis, Allen Witkowski, Anita Sengupta, 2009 .

Results of a 2000-Hour Wear Test of the NEXIS Ion Engine

James E. Polk, Dan M. Goebel, Anita Sengupta, 2005 .

Recent Advances in Nuclear Powered Electric Propulsion for Space Exploration

James E. Polk, Michael G. Houts, Anita Sengupta, 2008 .

VHITAL-160 thruster development status

Anita Sengupta, Colleen Marrese-Reading, Rich Hofer, 2006 .

An Evaluation of the Discharge Chamber of the 30,000 Hr Life Test of the Deep Space 1 Flight Spare Ion Engine

Anita Sengupta, Charles E. Garner, James Kulleck, 2004 .

An Overview of the VHITAL Program: A Two-Stage Bismuth Fed Very High Specific Impulse Thruster with Anode Layer

Azer P. Yalin, Anita Sengupta, Colleen Marrese-Reading, 2005 .

Supersonic Testing of 0.8 m Disk Gap Band Parachutes in the Wake of a 70 Deg Sphere Cone Entry Vehicle

Allen Witkowski, Thomas Jones, Anita Sengupta, 2009 .

The VHITAL Program to Demonstrate the Performance and Lifetime of a Bismuth-Fueled Very High Isp Hall Thruster

Michael Keidar, Anita Sengupta, Colleen Marrese-Reading, 2005 .

Ringsail parachutes for Planetary Entry Applications

Ricardo Machin, Anita Sengupta, Rob Sinclair, 2011, 2011 Aerospace Conference.

Cold atom laboratory mission system design

Anita Sengupta, Melissa Soriano, David Aveline, 2014, 2014 IEEE Aerospace Conference.

Very High Isp Thruster with Anode Layer (VHITAL): An Overview

Anita Sengupta, Colleen Marrese-Reading, Iain D. Boyd, 2004 .

Entry, Descent and Landing Systems Analysis Study: Phase 1 Report

David J. Kinney, Anita Sengupta, Alicia M. Dwyer-Cianciolo, 2010 .

Performance and Wear Test Results for a 20 kW-Class Ion Engine with Carbon-Carbon Grids

Dan M. Goebel, Anita Sengupta, Analyn C. Schneider, 2005 .

Supersonic Disk Gap Band Parachute Performance in the Wake of a Viking-Type Aeroshell from Mach 2 to 2.5

Anita Sengupta, Al Witkowski, Mark P. Wernet, 2008 .

Performance characteristics of the deep space 1 flight spare ion thruster long duration test, the first 21,300 hours of operation

John R. Anderson, James S. Sovey, Vincent K. Rawlin, 2002 .

Performance of a Subscale CPAS Conical Ribbon Drogue Parachute in a Turbulent Wake

Anita Sengupta, 2013 .

Summary of the VHITAL Thruster Technology Demonstration Program: A Two-Stage Bismuth-Fed Very High Specific Impulse TAL

Anita Sengupta, Colleen Marrese-Reading, Kurt A. Polzin, 2007 .

Subscale Test Program for the Orion Conical Ribbon Drogue Parachute

Robert Sinclair, Ricardo Machin, Gary Bourland, 2011 .

Findings from the supersonic qualification program of the Mars Science Laboratory parachute system

Allen Witkowski, Graham V. Candler, Carlos Pantano, 2009 .

Overview of the Mars Science Laboratory Parachute Decelerator System

Joe Morris, Mike Kandis, Keith Baker, 2007 .

Wear characteristics from the extended lift test of the DS1 flight spare ion thruster

John R. Brophy, Anita Sengupta, K. D. Goodfellow, 2003 .

The Exploration of Mars: Crew Surface Activities

Madhu Thangavelu, Aaron Kiely, Michael Myers, 2000 .

Fluid Structure Interaction of Parachutes in Supersonic Planetary Entry

Anita Sengupta, 2011 .

Supersonic Delta Qualification by Analysis Program for the Mars Science Laboratory Parachute Decelerator System

Graham V. Candler, Carlos Pantano, Anita Sengupta, 2007 .

Post-test analysis of the Deep Space 1 spare flight thruster ion optics

John R. Anderson, John R. Brophy, Anita Sengupta, 2004 .

Herakles Thruster Development for the Prometheus JIMO Mission

Michael J. Patterson, Anita Sengupta, Fred Elliott, 2005 .

Origins Space Telescope: trades and decisions leading to the baseline mission concept

David Yanatsis, David C. Redding, Charles Lawrence, 2021, Journal of Astronomical Telescopes, Instruments, and Systems.

A high power ion thruster for deep space missions.

Anita Sengupta, D. Goebel, J. Polk, 2012, The Review of scientific instruments.

Deep Space 1 Flight Spare Ion Thruster 30,000-Hour Life Test

John R. Brophy, Anita Sengupta, Charles E. Garner, 2009 .

Sensitivity Testing of the NSTAR Ion Thruster

John R. Brophy, Anita Sengupta, J. Brophy, 2007 .

Discharge Chamber Performance of the NEXIS Ion Thruster

James E. Polk, Dan M. Goebel, Anita Sengupta, 2004 .

Entry descent and landing on Mars

Anita Sengupta, A. Sengupta, 2013 .

Vibration test and analysis of the NEXIS ion engine

Anita Sengupta, John Steven Snyder, John S. Beatty, 2005 .

Vibration Test and Analysis of a 20-kW-Class Ion Engine

Anita Sengupta, John Steven Snyder, John S. Beatty, 2005 .

Explosive erosion during the Phoenix landing exposes subsurface water on Mars

Raymond E. Arvidson, Mark T. Lemmon, Anita Sengupta, 2011 .

PERFORMANCE CHARACTERISTICS OF THE DEEP SPACE 1 FLIGHT SPARE ION THRUSTER LONG DURATION TEST AFTER 21,300 HOURS OF OPERATION

James S. Sovey, John R. Brophy, Anita Sengupta, 2003 .

Supersonic Performance of Disk-Gap-Band Parachutes Constrained to a 0-Degree Trim Angle

Mike Kandis, Allen Witkowski, Anita Sengupta, 2009 .