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Space Shuttle Discovery as it approaches the International Space Station during the STS-114 on 28 July 2005. The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the extreme 1,650 °C (3,000 °F) heat of atmospheric reentry. A secondary goal was to protect from the heat and cold of ...
On the Space Shuttle, a support ring welded to the forward end of the nozzle is the engine attach point to the orbiter-supplied heat shield. Thermal protection is necessary because of the exposure portions of the nozzles experience during the launch, ascent, on-orbit and entry phases of a mission.
The Space Shuttle is a retired, ... the reusability of the orbiter required a multi-use heat shield. ... nose cone, and rocket nozzle. The solid-propellant motor ...
Many problems arose with the tiles used on the Space Shuttle, while minor damage to the heat shield was somewhat commonplace. Major damage to the heat shield almost caused the destruction of Space shuttle Atlantis in 1988 and did cause the loss of Columbia in 2003. [18] [19] [20]
UA120 was a family of American solid rocket boosters, ... necessary for crewed rockets such as the Space Shuttle or Manned Orbiting ... the nozzle, and a heat shield ...
The R-bar pitch maneuver (RPM), popularly called the rendezvous pitch maneuver or backflip, [1] was a maneuver performed by the Space Shuttle as it rendezvoused with the International Space Station (ISS) prior to docking. The Shuttle performed a backflip that exposed its heat-shield to the crew of the ISS that made photographs of it. Based on ...
In spacecraft design, a Sun shield restricts or reduces heat caused by sunlight hitting a spacecraft. [5] An example of use of a thermal shield is on the Infrared Space Observatory. [5] The ISO sunshield helped protect the cryostat from sunlight, and it was also covered with solar panels. [6]
Figure 1: A de Laval nozzle, showing approximate flow velocity increasing from green to red in the direction of flow Density flow in a nozzle. A rocket engine nozzle is a propelling nozzle (usually of the de Laval type) used in a rocket engine to expand and accelerate combustion products to high supersonic velocities.