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180° Ogive Panel Installed on Orion

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Technicians on work platforms monitor the progress as a crane brings the third of four Ogive panels closer for installation on Orion's Launch Abort System inside the Launch Abort System Facility at NASA’s Kennedy Space Center in Florida. The panels will smooth the airflow over the conical spacecraft to limit sound and vibration, which will make for a much smoother ride for the astronauts who will ride inside Orion in the future. The work marked the final major assembly steps for the spacecraft before it is transported to Space Launch Complex 37 at Cape Canaveral Air Force Station in November. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted flight test of Orion is scheduled to launch in December 2014 atop a United Launch Alliance Delta IV Heavy rocket, and in 2018 on NASA’s Space Launch System rocket.

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ksc 2014 4256 kennedy space center ogive panel ogive panel orion high resolution nasa
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Date

13/10/2014
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NASA
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https://images.nasa.gov/
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Public Domain Dedication (CC0)

label_outline Explore Ogive Panel, Ogive, Panel

CAPE CANAVERAL, Fla. -- Technicians in the Vehicle Assembly Building at NASA’s Kennedy Space Center in Florida, are jacking crawler-transporter 2, or CT-2, four feet off the floor to facilitate removal of the roller bearing assemblies. After inspections, new assemblies will be installed. The Ground Systems Development and Operations Program office at Kennedy is overseeing the upgrades to CT-2 so that it can carry NASA’s Space Launch System heavy-lift rocket and new Orion spacecraft to the launch pad. For more than 45 years the crawler-transporters were used to transport the mobile launcher platform and the Apollo-Saturn V rockets and, later, space shuttles to Launch Pads 39A and B. Photo credit: NASA/Charisse Nahser KSC-2013-1930

ORION Project-(SPLASH) Structural Passive Landing Attenuation fo

Steve Highly, left, Jim Hollinger, center, and Allen Rose calibrate SSM/I radiometers in the Image Processing Facility at the Naval Research Laboratory (NRL). Radiometers mounted aboard a RP-3A Orion aircraft will be used to validate data obtained through the Defense Meteorological Satellite Program (DMSP), a joint Navy/Air Force project

NASA's Lunar Reconnaissance Orbiter (LRO) POP + CATCH TEST + SOLAR PANEL

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S123E006246 - STS-123 - ISL Interface Panel on Node 2 taking during STS-123 / Expedition 16 Joint Operations

A member of Patrol Squadron 23 (VP-23) mans a radar console at sensor station No. 3 aboard a P-3 Orion aircraft

CAPE CANAVERAL, Fla. – A view from above inside the Operations and Checkout Building high bay at NASA’s Kennedy Space Center in Florida, shows the service module for the Orion spacecraft secured to a work stand. Technicians are preparing the three fairings for installation around the service module. The Orion spacecraft is being prepared for its first unpiloted flight test, Exploration Flight Test-1, or EFT-1, scheduled for launch atop a Delta IV rocket in September 2014. The Orion spacecraft is designed to carry astronauts to destinations not yet explored by humans. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. Orion is scheduled to launch atop NASA’s Space Launch System rocket in 2017. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Daniel Casper KSC-2013-4524

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the background, Paul Ogletree observes the monitor. Attached to the leading edge of the wing of the orbiters, the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

STS100-391-024 - STS-100 - Panel PMA2/02-05 with launch restraint fitting F11 taken during STS-100

NASA's Lunar Reconnaissance Orbiter (LRO) spacecraft / SOLAR PANEL INSTALL

NASA's Lunar Reconnaissance Orbiter (LRO) spacecraft / SOLAR PANEL INSTALL

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ksc 2014 4256 kennedy space center ogive panel ogive panel orion high resolution nasa