The NASA Engineering and Safety Center (NESC) is an independent engineering analysis and test organization providing support across the range of NASA programs. In 2007 NASA was developing the launch escape system for the Orion spacecraft that was evolved from the traditional tower-configuration escape systems used for the historic Mercury and Apollo spacecraft. The NESC was tasked, as a programmatic risk-reduction effort to develop and flight test an alternative to the Orion baseline escape system concept. This project became known as the Max Launch Abort System (MLAS), named in honor of Maxime Faget, the developer of the original Mercury escape system. Over the course of approximately two years the NESC performed conceptual and tradeoff an...
The National Aeronautics and Space Administration created the Constellation program to develop the n...
One of the primary design drivers for NASA's Crew Exploration Vehicle (CEV) is to ensure crew safety...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...
The NASA Engineering and Safety Center initiated the Max Launch Abort System (MLAS) Project to inves...
In 2007, the NASA Engineering and Safety Center (NESC) initiated the Max Launch Abort System Project...
In 2007, the NASA Exploration Systems Mission Directorate (ESMD) chartered the NASA Engineering Safe...
The NASA Orion Flight Test Office was tasked with conducting a series of flight tests in several lau...
The NASA Orion Flight Test Office was tasked with conducting a series of flight tests in several lau...
This paper describes initial flight performance analyses conducted early in the Orion Project to sup...
The Orion Crew Exploration Vehicle is America’s next generation of human rated space-craft. The Orio...
This presentation provides a concise overview of the highly successful Orion Pad Abort 1 (PA-1) flig...
This paper covers the simulation and evaluation of a controller design for the Crew Module (CM) Laun...
The flight control system for the NASA Space Launch System (SLS) employs a control architecture that...
NASA formed the NASA Engineering and Safety Center in 2003 following the Space Shuttle Columbia acci...
Overview of the current Orion Escape System in relation to its historical technological heritage
The National Aeronautics and Space Administration created the Constellation program to develop the n...
One of the primary design drivers for NASA's Crew Exploration Vehicle (CEV) is to ensure crew safety...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...
The NASA Engineering and Safety Center initiated the Max Launch Abort System (MLAS) Project to inves...
In 2007, the NASA Engineering and Safety Center (NESC) initiated the Max Launch Abort System Project...
In 2007, the NASA Exploration Systems Mission Directorate (ESMD) chartered the NASA Engineering Safe...
The NASA Orion Flight Test Office was tasked with conducting a series of flight tests in several lau...
The NASA Orion Flight Test Office was tasked with conducting a series of flight tests in several lau...
This paper describes initial flight performance analyses conducted early in the Orion Project to sup...
The Orion Crew Exploration Vehicle is America’s next generation of human rated space-craft. The Orio...
This presentation provides a concise overview of the highly successful Orion Pad Abort 1 (PA-1) flig...
This paper covers the simulation and evaluation of a controller design for the Crew Module (CM) Laun...
The flight control system for the NASA Space Launch System (SLS) employs a control architecture that...
NASA formed the NASA Engineering and Safety Center in 2003 following the Space Shuttle Columbia acci...
Overview of the current Orion Escape System in relation to its historical technological heritage
The National Aeronautics and Space Administration created the Constellation program to develop the n...
One of the primary design drivers for NASA's Crew Exploration Vehicle (CEV) is to ensure crew safety...
The implementation of a new dispersion methodology is described, which dis-perses abort initiation a...