Add to ORKGRadio frequency transmission characteristics of ablation materials for planetary entry vehicle heat shield
In 2012, NASA's mission of landing the Mars Science Laboratory (MSL) on Mars was successful. MSL was...
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Ablative heat shield materials for Mars atmosphere entry evaluated for RF transmission loss and flex...
Transmission loss and effects on antenna radiation patterns and impedance produced by thermally degr...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Entering a planetary atmosphere is one of the most claim missions as the space probe faces a loss of...
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Hypersonic spacecraft reentering the earth's atmosphere encounter extreme heat due to atmospheric fr...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight tes
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
Facilities for simulating entry environment and response of ablative materials to simulated entry en...
Nose cone mounted heat resistant antenna comprising plurality of adjacent layers of silica not intro...
In 2012, NASA's mission of landing the Mars Science Laboratory (MSL) on Mars was successful. MSL was...
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...
Ablative heat shield materials for Mars atmosphere entry evaluated for RF transmission loss and flex...
Transmission loss and effects on antenna radiation patterns and impedance produced by thermally degr...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
Entering a planetary atmosphere is one of the most claim missions as the space probe faces a loss of...
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Hypersonic spacecraft reentering the earth's atmosphere encounter extreme heat due to atmospheric fr...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight tes
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
Facilities for simulating entry environment and response of ablative materials to simulated entry en...
Nose cone mounted heat resistant antenna comprising plurality of adjacent layers of silica not intro...
In 2012, NASA's mission of landing the Mars Science Laboratory (MSL) on Mars was successful. MSL was...
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Design and development of sensors for measuring ablative changes in space vehicle heat shield during...