Air Radiation Analysis of a Superorbital Reentry Vehicle
Analysis of Rarefaction Effects in the Hypersonic Rarefied Wind Tunnel
ANALYSIS OF SHOCK LAYER RADIATION IN VACUUM-ULTRAVIOLET REGION FOR HAYABUSA RETURN CONDITIONS
An Experimental Study on Thermal Response of Low Density Carbon-Phenolic Ablators
ARCJET TESTINGS OF SILICA AEROGEL TOWARD MARS AEROFLYBYSAMPLE COLLECTION MISSION
Development of an Aerogel Sample Collector for Martian Dust Sample Return (AIAA 2014-2382)
Effects of piston profiles on oil film behavior by means of LIF/PIV
ELECTRONIC EXCITATION MODELING FOR INDUCTIVELY COUPLED PLASMA FLOWS
Experimental and Computational Investigation of Rarefied Hypersonic Aerodynamics (AIAA 2014-1214)
Experimental and Numerical Study of Flow Diagnostics in Hypersonic Rarefied Wind Tunnel in JAXA
Experimental and Numerical Study of Thermal Response of Ablator in an Arc-Jet Facility AIAA Paper
Experimental Investigations of Rovibrational Temperatures Derived from Different Electronic State
FEASIBILITY ASSESSMENT OF NONSTOP MARS SAMPLE RETURN SYSTEM
MODELING OF MARTIAN DUST COLLECTION FOR NON-STOP MARS SAMPLE RETURN MISSION
Nonstop Mars Sample Return System Using Aerocapture Technologies
Numerical Analysis of Aerodynamic Heating on MUSES-C Reentry Capsule
Numerical Analysis of Graphite Ablation in Nitrogen Flow
OPTICAL TRACKING AND SPECTROSCOPIC MEASUREMENT OF HAYABUSA CAPSULE REENTRY FIREBALL
Post-Flight Analysis of Hayabusa; Asteroid Sample Return Capsule (AAS 12-579)
PREDICTION ACCURACY OF THERMAL RESPONSE OF ABLATOR UNDER ARCJET FLOW CONDITIONS
Study of Hybrid Dust Sample Collection System Toward Mars Aeroflyby Sample Collection Mission
Study of Micron-sized Martian Dust Sample Capture Using Aerogel
Study of Nitrogen Recombination Coefficient for SiC Material Surfaces