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NASA - Thermal Protection System (TPS) and Materials

Space vehicles that enter a planetary atmosphere (i.e. earth) like the Space Shuttle Orbiter require the use of a thermal protection system (TPS) to protect them from aerodynamic heating. The aerodynamic heating is generated at the surface of an entering object due to the combination of compression

Thermal Protection Systems - NASA

Thermal Protection System. Thermal Protection System Could Take the Heat Orbiter remained protected during catalytic heating. Flow Nitrogen and oxygen molecules are dissociated in the shock layer. Atoms may recombine and form molecules on the vehicle surface. Oxygen molecules in the shock layer separate into O+ and O-atoms. Recombination of

Space Shuttle thermal protection system - Wikipedia

The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the searing 1,650 °C (3,000 °F) heat of atmospheric reentry.A secondary goal was to protect from the heat and cold of space while in orbit.

4 THERMAL PROTECTION SYSTEM - The National Academies Press

The thermal protection system (TPS) for the RLV must protect the structure and cryogenic fuel tanks from extremely high temperatures during launch and reentry. To meet the requirements of an RLV, the TPS must be readily producible, lightweight, operable, and reusable with a minimum lifetime of 100

Aerospace | Thermal Protection | Momentive

Momentive produces a wide range of materials used in thermal protection systems. Our RTV silicones consist of rubber and gel products developed for adhesion, sealing, coating and encapsulation/ potting applications. The Si-O backbone of silicones provides excellent temperature performance, both high temperature stability and low temperature

Thermal Protection Systems | Textron Systems

Weapon & Sensor Systems has a notable heritage in aerospace materials research, development and manufacturing. These thermal protection materials kept America’s astronauts safe during re-entry for NASA’s Apollo program.

Atmospheric entry - Wikipedia

Thermal protection systems. A thermal protection system or TPS is the barrier that protects a spacecraft during the searing heat of atmospheric reentry. A secondary goal may be to protect the spacecraft from the heat and cold of space while in orbit. Multiple approaches for the thermal protection of spacecraft are in use, among them ablative

Thermal Protection Systems? - NASA

Entry Systems & Technology Program Antenn a Afterbody Heat Sink Heat protection and structural system Trajectory Control Jets Trajectory Control System Data Capsule (recoverable) Mark 2 Re-Entry Vehicle Telemetry and Instrumentatio n •Absorbs, dissipates heat from other objects in contact •First type of re-entry thermal protection system

Thermal Protection Systems - University Of Maryland

Thermal Protection Systems ENAE 791 - Launch and Entry Vehicle Design U N I V E R S I T Y O F MARYLAND Term Project - Top Level Requirements • Design a system to allow the construction of one


Because the thermal protection system is installed on the outside of the orbiter skin, it establishes the aerodynamics over the vehicle in addition to acting as the heat sink. Orbiter interior temperatures also are controlled by internal insulation, heaters and purging techniques in the various phases of the mission.

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