Jet Propulsion Laboratory JPL Earth JPL Solar System JPL Stars and Galaxies JPL Science and Technology MRO Home NASA Home Page Jet Propulsion Laboratory California Institute of Technology Follow this link to skip to the main content
Jet Propulsion Laboratory
+ NASA Homepage
+ NASA en Español
+ Marte en Español
Search Mars
Go Search
Mars Reconnaissance Orbiter
Overview Science Technology The Mission People Features Events Multimedia
Mars for Kids
Mars for Students
Mars for Educators
Mars for Press
+ Mars Home
+ MRO Home
The Mission
Summary
Where is MRO now?
Mission Team
Launch Vehicle
Summary
Payload Adapter
Stage I Atlas Booster
Payload Fairing
Stage II Centaur Upper Stage Booster
Spacecraft
Mission Timeline
Communications with Earth
Payload Fairing

LAUNCH VEHICLE COMPONENTS
Summary | Payload Adapter | Stage I Atlas Booster | Payload Fairing | Stage II Centaur Upper Stage Booster

Mars Reconnaissance Orbiter used a payload fairing (nose cone) that was 4 meters (13 feet) in diameter and weighed about the same as the spacecraft.

The fairing protected the spacecraft from the weather on the ground as well as from the atmosphere during flight. While the launch vehicle was on the launch pad, air conditioning was supplied to the spacecraft to control temperature and protect it from dust and dirt.

Shortly after Centaur ignition, the fairing was no longer needed and was separated into its two halves by explosive bolts and jettisoned. Automatic timers in the Centaur controlled this operation. The two fairing halves swung away to either side of the spacecraft and fell back to Earth, landing in the ocean.


Credits Feedback Related Links Sitemap
USA Gov
NASA Logo