This paper presents recent experimental results from arc-jet tests of the Orion heatshield that were conducted at NASA Ames Research Center. Test conditions that simulated a set of heating profiles in time representative of the Orion flight environments were used to observe their effect on Orion's block architecture in terms of differential recession or fencing. Surface recession of arc-jet models was characterized during and after testing to derive fencing profiles used for the baseline sizing of the heatshield. Arc-jet test data show that the block architecture produces varying degrees of fencing
This presentation was part of the session : Current Planetary Probe Science and TechnologySixth Inte...
This course will cover an overview of the Entry Systems and Technology Division (TS) at NASA Ames Re...
The aerodynamic effects of the recession of the ablative thermal protection system for the Orion Com...
NASA's new Laser-Enhanced Arcjet Facility (LEAF) employs 200 kilowatts of continuous-wave fiber lase...
The Orion Multi-Purpose Crew Vehicle will one day carry astronauts to the Moon and beyond, and Orion...
This paper presents the first set of experimental results from Laser Enhanced Arc-Jet Facility (LEAF...
A new approach for arc jet testing of thermal protection materials at conditions approximating the t...
The reaction control system jets of the Orion Multi Purpose Crew Vehicle can have a significant impa...
The paper describes the consolidation of NASA's high powered arc-jet testing at a single location. T...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
Tests were performed to demonstrate the feasibility of a new method of measuring surface recession o...
For the Orion Multi-Purpose Crew Vehicle (MPCV) project, NASA is minimizing the use of onboard diagn...
This paper reports computational analyses in support of two wedge tests in a high enthalpy arc-jet f...
An experimental study has been conducted to assess the effects of compression pad cavities on the ae...
This paper reports computational simulations and analysis in support of calibration and flow charact...
This presentation was part of the session : Current Planetary Probe Science and TechnologySixth Inte...
This course will cover an overview of the Entry Systems and Technology Division (TS) at NASA Ames Re...
The aerodynamic effects of the recession of the ablative thermal protection system for the Orion Com...
NASA's new Laser-Enhanced Arcjet Facility (LEAF) employs 200 kilowatts of continuous-wave fiber lase...
The Orion Multi-Purpose Crew Vehicle will one day carry astronauts to the Moon and beyond, and Orion...
This paper presents the first set of experimental results from Laser Enhanced Arc-Jet Facility (LEAF...
A new approach for arc jet testing of thermal protection materials at conditions approximating the t...
The reaction control system jets of the Orion Multi Purpose Crew Vehicle can have a significant impa...
The paper describes the consolidation of NASA's high powered arc-jet testing at a single location. T...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
Tests were performed to demonstrate the feasibility of a new method of measuring surface recession o...
For the Orion Multi-Purpose Crew Vehicle (MPCV) project, NASA is minimizing the use of onboard diagn...
This paper reports computational analyses in support of two wedge tests in a high enthalpy arc-jet f...
An experimental study has been conducted to assess the effects of compression pad cavities on the ae...
This paper reports computational simulations and analysis in support of calibration and flow charact...
This presentation was part of the session : Current Planetary Probe Science and TechnologySixth Inte...
This course will cover an overview of the Entry Systems and Technology Division (TS) at NASA Ames Re...
The aerodynamic effects of the recession of the ablative thermal protection system for the Orion Com...