Peter Gage

发表

GENERALIZED VEHICLE PERFORMANCE CLOSURE MODEL FOR TWO -STAGE -TO -ORBIT LAUNCH VEHICLES

John Bradford, Min Qu, John Sohn, 2004 .

Application of Risk Informed Decision Making to a Highly Reliable Three Dimensionally Woven Thermal Protection System for Mars Sample Return

Peter Gage, Jacob T. Needels, Donald T. Ellerby, 2020 .

Development challenges of game-changing entry system technologies from concept to mission infusion

Paul Wercinski, Ethiraj Venkatapathy, Peter Gage, 2016, 2016 IEEE Aerospace Conference.

Representation Language for Evaluating Reusable Launch Vehicle Concepts

Peter Gage, Jeremy C. Vander Kam, P. Gage, 2004, J. Aerosp. Comput. Inf. Commun..

Rapid Geometry Creation for Computer-Aided Engineering Parametric Analyses

Peter Gage, Ted Manning, Veronica Hawke, 2007 .

Estimating Orion Heat Shield Failure Due To Ablator Cracking During The EFT-1 Mission

Peter Gage, Jeremy Vander Kam, 2016 .

LVL EDITOR: A GRAPHICAL TOOL FOR VISUALIZING AND MANAGING DATA IN AN ENGINEERING COMPONENT HIERARCHY

Xun Jiang, Peter Gage, Grant Palmer, 2004 .

Weights Analysis of Space Launch Vehicles in an Advanced Engineering Environment

Xun Jiang, Min Qu, Peter Gage, 2004 .

Current Testing Capabilities at the NASA Ames Ballistic Ranges

David W. Bogdanoff, Peter Gage, Tim Tam, 1999 .

Mission Assurance and Residual Risk: The Performance Verification Challenge for Technology Infusion

Ethiraj Venkatapathy, Peter Gage, 2017 .

ComGeom: A Geometry Representation and Data Sharing Tool for Analysis of Launch Vehicles

Chun Tang, Peter Gage, Veronica Hawke, 2005 .

Heatshield for Extreme Entry Environment Technology (HEEET) Development and Maturation Status for NF Missions

Milad Mahzari, Peter Gage, Donald T. Ellerby, 2016 .

Sonic boom testing of Artificially Blunted Leading Edge (ABLE) concepts in the NASA Ames aeroballistic range

David W. Bogdanoff, Leslie Yates, Stephen M. Ruffin, 2000 .

Enabling Venus In-Situ Science - Deployable Entry System Technology, Adaptive Deployable Entry and Placement Technology (ADEPT): A Technology Development Project funded by Game Changing Development Program of the Space Technology Program

Paul Wercinski, Dinesh K. Prabhu, Ethiraj Venkatapathy, 2012 .

A Loaf-Shaped Entry Vehicle for a Mars Airplane (The Best Thing Since Sliced Bread?)

Paul Wercinski, Chul B. Park, Peter Gage, 2000 .

Mars Sample Return Earth Entry Vehicle Design:can the Reliability Requirement Be Met by Emerging New Technologies?

Ethiraj Venkatapathy, Peter Gage, Keith Peterson, 2016 .

Summary of Adtt Website Functionality and Features

Peter Gage, Veronica Hawke, Scott Lawrence, 2013 .

Preliminary Assessment of a Neptune Aerocapture Mission Using an Integrated Design Tool

Paul Wercinski, Peter Gage, 1998 .

Aerospace Vehicle Trajectory Design and Optimization Within a Multi-Disciplinary Environment

David Saunders, Peter Gage, Robert Windhorst, 2004 .

Adaptable, Deployable Entry and Placement Technology (ADEPT) for Future Mars Missions

Paul Wercinski, Dinesh K. Prabhu, Gary A. Allen, 2013 .

Structures and Mechanisms Design Concepts for Adaptive Deployable Entry Placement Technology

Ethiraj Venkatapathy, James O. Arnold, Bryan Yount, 2013 .

A Top-down Risk Assessment Tool for a Reusable Launch Vehicle Development Program

Susie Go, Peter Gage, Donovan Mathias, 2003 .

Trajectory and Thermal Protection System Design for Reusable Launch Vehicles

Peter Gage, Jeffrey V. Bowles, Robert Windhorst, 2004 .

The Devil's in the Tails - Reliability Prediction Methodologies for the Orion Heat Shield

Peter Gage, Jeremy Vander Kam, Austin R. Howard, 2011 .

Evaluation of the NASA ARC Jet Capabilities to Support Mission Requirements

Anthony M. Calomino, Peter Gage, Judee Robey, 2013 .

Crew Transfer Vehicle trajectory optimization

David Saunders, Peter Gage, James Reuther, 2001 .

The Launch Vehicle Language Data Model Applied to Analysis Tool Connectivity

Peter Gage, Jeremy Vander Kam, J. Sohn, 2004 .

Aerospace Vehicle Trajectory Design and Optimization Within a Multi-Disciplinary Environment

Peter Gage, Robert Windhorst, Eric Lau, 2006, J. Aerosp. Comput. Inf. Commun..

A Web-based Analysis System for Planetary Entry Vehicle Design

Paul Wercinski, Ethiraj Venkatapathy, Peter Gage, 1998 .

AIAA 2001-2884 A Reusable Space Vehicle Design Study Exploring Sharp Leading Edges

David J. Kinney, David Saunders, Peter Gage, 2001 .

Adaptive Deployable Entry and Placement Technology (ADEPT): A Feasibility Study for Human Missions to Mars

David J. Kinney, Dinesh K. Prabhu, Ethiraj Venkatapathy, 2011 .