Overview and Performance of the Low-Earth Orbit Flight Test of an Inflatable Decelerator Instrumentation Suite

On November 10, 2022, NASA launched the Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) reentry vehicle as a secondary payload on an Atlas V launch vehicle from Vandenburg Space Force Base. The LOFTID technology demonstration mission successfully returned a 6-meter diameter, 70° sphere-cone Hypersonic Inflatable Aerodynamic Decelerator (HIAD) from low earth orbit. The LOFTID vehicle was instrumented with a suite of sensors that measured high-value science data at over 150 vehicle locations. Thermocouples embedded in the aeroshell monitored the temperature within the flexible thermal protection system and inflatable structure. Heat flux gauges and surface pressure transducers measured the conditions on the vehicle’s rigid nose. Loadcell pins measured the interface loads between the inflatable structure and the centerbody. Onboard visible light cameras and colocated infrared cameras captured a 360° view of structural deflection and temperature distribution on the aft side of the heatshield. The data collected by the LOFTID instrumentation suite enabled reconstruction of the aerodynamic, aerothermal, thermal, and structural performance of the vehicle and provide a wealth of information for the design of future HIAD missions. The LOFTID instrumentation, a summary of the in-flight performance, and examples of data products from the post-flight analysis effort are presented.

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Publication Details

Journal
Journal of Spacecraft and Rockets
Published
2025-04-11
DOI
https://doi.org/10.2514/1.a36287
Citations
2
Primary Topic
Planetary Science and Exploration
Type
article
Field-Weighted Citation Impact
2.31

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article

Overview and Performance of the Low-Earth Orbit Flight Test of an Inflatable Decelerator Instrumentation Suite

Ruth A. Miller, Gregory Swanson, Neil Cheatwood, Hannah S. Alpert et al.
2 citations
Journal of Spacecraft and Rockets
Planetary Science and Exploration
2.31
article

Overview and Performance of the Low-Earth Orbit Flight Test of an Inflatable Decelerator Instrumentation Suite

Ruth A. Miller, Gregory Swanson, Neil Cheatwood, Hannah S. Alpert, Cole Kazemba, Stephen J. Hughes, Joseph D. Williams
article en
2 citations

Abstract

On November 10, 2022, NASA launched the Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) reentry vehicle as a secondary payload on an Atlas V launch vehicle from Vandenburg Space Force Base. The LOFTID technology demonstration mission successfully returned a 6-meter diameter, 70° sphere-cone Hypersonic Inflatable Aerodynamic Decelerator (HIAD) from low earth orbit. The LOFTID vehicle was instrumented with a suite of sensors that measured high-value science data at over 150 vehicle locations. Thermocouples embedded in the aeroshell monitored the temperature within the flexible thermal protection system and inflatable structure. Heat flux gauges and surface pressure transducers measured the conditions on the vehicle’s rigid nose. Loadcell pins measured the interface loads between the inflatable structure and the centerbody. Onboard visible light cameras and colocated infrared cameras captured a 360° view of structural deflection and temperature distribution on the aft side of the heatshield. The data collected by the LOFTID instrumentation suite enabled reconstruction of the aerodynamic, aerothermal, thermal, and structural performance of the vehicle and provide a wealth of information for the design of future HIAD missions. The LOFTID instrumentation, a summary of the in-flight performance, and examples of data products from the post-flight analysis effort are presented.

Journal of Spacecraft and RocketsVol. 62(4)
Ames Research Center (US), Langley Research Center (US)
Ames Research Center
Openalex Percentile: Top 12%
Planetary Science and Exploration
2.31
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Overview and Performance of the Low-Earth Orbit Flight Test of an Inflatable Decelerator Instrumentation Suite — Ruth A. Miller, Gregory Swanson, et al. · Journal of Spacecraft and Rockets (2025) | TGRS Research Map | TGRS