Reentry analysis is essential to understanding the consequences of the full life cycle of a spacecraft. Since reentry is a key factor in spacecraft development, NASA and ESA have separately developed tools to assess the survivability of objects during reentry. Criteria such as debris casualty area and impact energy are particularly important to understanding the risks posed to people on Earth. Therefore, NASA and ESA have undertaken a series of comparison studies of their respective reentry codes for verification and improvements in accuracy. The NASA Object Reentry Survival Analysis Tool (ORSAT) and the ESA Spacecraft Atmospheric Reentry and Aerothermal Breakup (SCARAB) reentry analysis tools serve as standard codes for reentry survivabili...
This paper describes the functionality and use of ORDEM2010, which replaces ORDEM2000, as the NASA O...
The limited availability of data for satellite fragmentations and debris in the geosynchronous orbit...
[EN] Space debris that re-enter the Earth's atmosphere can be partially or fully ablated along the t...
The Object Reentry Survival Analysis Tool (ORSAT) has been used in the NASA Orbital Debris Program O...
In the past 40 years, thousands of objects have been placed in Earth orbit and are being tracked. Sp...
The NASA Orbital Debris Program Office (ODPO) studies all aspects of spacecraft end-of-life and orbi...
The key risk analysis technologies for the re-entry of space objects into Earth`s atmosphere are div...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
AbstractThe reentry of uncontrolled spacecraft may be broken into many pieces of debris at an altitu...
This paper explores the differences between, and shares the lessons learned from, two hypervelocity ...
Since the Second European Conference on Space Debris in 1997, the Orbital Debris Program Office at t...
To replicate a hyper-velocity fragmentation event using modern-day spacecraft materials and construc...
Existing DoD and NASA satellite breakup models are based on a key laboratory-based test, Satellite O...
The NASA Orbital Debris Program Office has developed the Orbital Debris Engineering Model (ORDEM) pr...
This paper describes the functionality and use of ORDEM2010, which replaces ORDEM2000, as the NASA O...
The limited availability of data for satellite fragmentations and debris in the geosynchronous orbit...
[EN] Space debris that re-enter the Earth's atmosphere can be partially or fully ablated along the t...
The Object Reentry Survival Analysis Tool (ORSAT) has been used in the NASA Orbital Debris Program O...
In the past 40 years, thousands of objects have been placed in Earth orbit and are being tracked. Sp...
The NASA Orbital Debris Program Office (ODPO) studies all aspects of spacecraft end-of-life and orbi...
The key risk analysis technologies for the re-entry of space objects into Earth`s atmosphere are div...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
AbstractThe reentry of uncontrolled spacecraft may be broken into many pieces of debris at an altitu...
This paper explores the differences between, and shares the lessons learned from, two hypervelocity ...
Since the Second European Conference on Space Debris in 1997, the Orbital Debris Program Office at t...
To replicate a hyper-velocity fragmentation event using modern-day spacecraft materials and construc...
Existing DoD and NASA satellite breakup models are based on a key laboratory-based test, Satellite O...
The NASA Orbital Debris Program Office has developed the Orbital Debris Engineering Model (ORDEM) pr...
This paper describes the functionality and use of ORDEM2010, which replaces ORDEM2000, as the NASA O...
The limited availability of data for satellite fragmentations and debris in the geosynchronous orbit...
[EN] Space debris that re-enter the Earth's atmosphere can be partially or fully ablated along the t...