The NASA Engineering and Safety Center (NESC) was requested to establish the Simulation Framework for Rapid Entry, Descent, and Landing (EDL) Analysis assessment, which involved development of an enhanced simulation architecture using the Program to Optimize Simulated Trajectories II (POST2) simulation tool. The assessment was requested to enhance the capability of the Agency to provide rapid evaluation of EDL characteristics in systems analysis studies, preliminary design, mission development and execution, and time-critical assessments. Many of the new simulation framework capabilities were developed to support the Agency EDL Systems Analysis (EDL-SA) team, that is conducting studies of the technologies and architectures that are required...
The future exploration of the Solar System will require innovations in transportation and the use of...
This presentation was part of the session : Strategic PerspectivesSixth International Planetary Prob...
Crew Exploration Vehicle (CEV) Chief Engineer requested a risk comparison of the Integrated Landing ...
The NASA Engineering and Safety Center (NESC) was requested to establish the Simulation Framework fo...
Entry, Descent and Landing (EDL) Modeling and Simulation (MS) is an enabling capability for complex ...
The Entry Systems Modeling (ESM) technology development project, initiated in 2012 under NASAs Game ...
A description of the Engineering Design Integration (EDIN) Simulation System as it exists at Johnson...
Because Entry, Descent and Landing (EDL) system validations are limited in Earth environments, these...
ESM (Entry Systems Modeling Project) is the only dedicated research effort for EDL (Entry, Descent a...
This NASA Engineering and Safety Center (NESC) assessment was established to develop a set of time h...
This paper describes a model-predictive automatic recovery system for aircraft on the verge of a los...
The NASA Engineering and Safety Center received a request from Mr. Daniel Murri (NASA Technical Fell...
This talk will provide an overview of investments in the Entry Systems Modeling project, along with ...
Crew Exploration Vehicle (CEV) water splashdowns were simulated in order to find maximum acceleratio...
With any space related mission, the unknown effects are often some of the most important design cons...
The future exploration of the Solar System will require innovations in transportation and the use of...
This presentation was part of the session : Strategic PerspectivesSixth International Planetary Prob...
Crew Exploration Vehicle (CEV) Chief Engineer requested a risk comparison of the Integrated Landing ...
The NASA Engineering and Safety Center (NESC) was requested to establish the Simulation Framework fo...
Entry, Descent and Landing (EDL) Modeling and Simulation (MS) is an enabling capability for complex ...
The Entry Systems Modeling (ESM) technology development project, initiated in 2012 under NASAs Game ...
A description of the Engineering Design Integration (EDIN) Simulation System as it exists at Johnson...
Because Entry, Descent and Landing (EDL) system validations are limited in Earth environments, these...
ESM (Entry Systems Modeling Project) is the only dedicated research effort for EDL (Entry, Descent a...
This NASA Engineering and Safety Center (NESC) assessment was established to develop a set of time h...
This paper describes a model-predictive automatic recovery system for aircraft on the verge of a los...
The NASA Engineering and Safety Center received a request from Mr. Daniel Murri (NASA Technical Fell...
This talk will provide an overview of investments in the Entry Systems Modeling project, along with ...
Crew Exploration Vehicle (CEV) water splashdowns were simulated in order to find maximum acceleratio...
With any space related mission, the unknown effects are often some of the most important design cons...
The future exploration of the Solar System will require innovations in transportation and the use of...
This presentation was part of the session : Strategic PerspectivesSixth International Planetary Prob...
Crew Exploration Vehicle (CEV) Chief Engineer requested a risk comparison of the Integrated Landing ...