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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.

NASA - Thermal Protection System (TPS) and Materials

The aerodynamic heating is generated at the surface of an entering object due to the combination of compression and surface friction of the atmospheric gas. The vehicle's configuration and entry trajectory in combination with the type of thermal protection system used define the temperature distribution on the vehicle.

Thermal Protection Systems - NASA

Thermal Protection Systems Introduction Gail Chapline Orbiter Thermal Protection System Alvaro Rodriguez and this thermal shield demanded both light weight and low cost. The shuttle Thermal Protection System development efforts, ablatives and hot structures were the early competitors.

Thermal Protection Systems | Ultramet

Thermal Protection System Aerogel-filled Foam Insulation. Ultramet fills an open-cell foam skeleton with ultralow-density aerogel to create a highly insulating and lightweight foam-core thermal protection material that can be economically fabricated into large and complex shapes.

Lesson Thermal Protection Systems: Day 1 | BetterLesson

Designing thermal protection systems also can provide students with practice in Cross Cutting Concepts of “Systems and Models” as well as “Energy and Matter”. Students use the thermal protections systems as a model that can show the input and output of energy and track how energy flows within the system (CCC Systems and Models).

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

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

Thermal Protection Systems | Textron Systems

Thermal Protection Systems. Thermal coatings with large and/or complex shapes for a variety of specialized applications. Qualifications of adhesively bonded assemblies. These thermal protection materials kept America’s astronauts safe during re-entry for NASA’s Apollo program.

Atmospheric entry - Wikipedia

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.


THERMAL PROTECTION SYSTEM The thermal protection system consists of various materials applied externally to the outer structural skin of the orbiter to maintain the skin within acceptable temperatures, primarily during the entry phase of the mission. The orbiter's outer structural skin is constructed primarily of aluminum and graphite epoxy.

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