A UNITED LAUNCH ALLIANCE ATLAS-V TO LAUNCH NROL-67 CLASSIFIED PAYLOAD.
Photo Credit & Copyright: United Launch Alliance (ULA): CLICK photo for larger view and look below for related information and data links on the mission and where to stream live.
LAUNCH ALERT: (Delayed from March 25)
Thursday, April 10, at 1745 UTC (1345 EDT & 1045 PDT) a United Launch Alliance (ULA) Atlas V-541 Rocket designated (AV-045) will be launching (NROL-67); a classified payload for the United States Naval Reconnaissance Office (NRO) from Space Launch Complex-41 (SLC-41 or SLICK-41) at the Cape Canaveral Air Force Station (CCAFS).
It’s likely that because of the classified nature of this launch the live feed will cut off before payload fairing separation but liftoff and incipient stage of the flight will still be shown. This will also be ULA’s 80th flight but only the second flight ever for the Atlas-V-541 configuration. The only other 541 flight was for Mars Science Lab (MSL) Curiosity.
The Atlas-5 (V) 500 Series rocket is a two-stage rocket that depending on the size of the fairing used stands between 59.7 m (196 ft.) and 65.5 m (215 ft.) with a diameter of 12.5ft (3.81m) and consists of an Atlas Common Core Booster with a Russian RD-180 engine and first stage with a United States RL-10 Centaur upper stage built by AeroJet-Rocketdyne. The vehicle is available in 6 different configurations which are built specifically for each individual mission. Its launch sites are Cape Canaveral Air Force Station (CCAFS), Launch Complex-41 (LC-41) or Vandenberg Air Force Base, Launch Complex-3 (LC-3). Performance to Geosynchronous Transfer Orbit (GTO) ranges from 8,320 lb. to 19,620 lb. Performance to Low Earth Orbit (LEO) ranges from 17,510 lb. to 40,800 lb.
541 DESIGNATION CONFIGURATION SUMMARY:
5 = 5 Meter fairing (2-shell).
4 = 4 External solid rocket boosters.
1 = 1 Centaur second stage engine.
MAIN PAYLOAD FAIRING (PLF): The Main Payload Fairing for the Atlas-V-542 is a two-shell, 5 m (17.8 ft.) diameter fairing and is used to protect the spacecraft & Centaur during its ascent through atmospheric turbulence and into space. Once safely out of Earth’s atmosphere (Or at least most of it), the fairing is pyrotechnically jettisoned via a debris-free actuating system.
CENTAUR UPPER STAGE: The Centaur Upper stage is 3.1 m (10 ft.) in diameter and 12.7 m (41.6 ft.) in length. It consists of a single Cryogenic RL-10A-4-2 (RL-10) Aerojet Rocketdyne Engine that provides 22,300 lb. of thrust and utilizes liquid hydrogen (LH2) for propellant and liquid oxygen (LOX) as an oxidizer with a burn time of up to 740 seconds to include multiple engine firings. There are also four 27-N (Newton) thrusters and eight 40-N (Newton) thrusters used for attitude control. Both utilize hydrazine as propellant. The Centaur Forward Adapter (CFA) provides structural mountings for vehicle electronics within the spacecraft.
SOLID ROCKET BOOSTERS (SRB’s): Have a diameter of 158 cm (62.2 in) and a length of 20 m (65.6 ft.). The total number of SRB’s utilized is dependent on the individual mission and vary from none at all to 5. They are jettisoned after approximately a minute and a half of flight.
COMMON CORE BOOSTER (CCB) (First-Stage): The American Atlas-V Common Booster Core is 106.5 ft. (32.46 m) in length by 12.5 ft. (3.8 m) in diameter and is powered by a single two-chamber Russian RD-180 engine that utilizes Rocket Propellant-1 (RP-1 or highly purified kerosene) as propellant and Liquid Oxygen (LOX) as the oxidizer. It provides 860,300lb. of thrust at sea level and can burn for 253 seconds. The RD-180 engine is modeled after the 4-chanber RD-170 engines used by the Zenit rocket family.
ULA NROL-67 MISSION:
ULA NROL 67: http://www.ulalaunch.com/site/pages/Launch.shtml#/48/
Spaceflight 101 NROL-67: http://www.spaceflight101.com/atlas-v-nrol-67-launch-updates.html
Spaceflight Now NROL-67: http://spaceflightnow.com/atlas/av045/infosheet.html
UNITED LAUNCH ALLIANCE (ULA):
ULA homepage: http://www.ulalaunch.com/site/default.shtml
Atlas V rocket: http://www.ulalaunch.com/site/pages/Products_AtlasV.shtml
Atlas V Users Guide: http://www.ulalaunch.com/site/docs/product_cards/guides/AtlasVUsersGuide2010.pdf?bcsi_scan_df193da5ba4c5bc6=0&bcsi_scan_filename=AtlasVUsersGuide2010.pdf
Atlas V Product Card: http://www.ulalaunch.com/site/docs/product_cards/AV_product_card.pdf
Atlas V 500 Series Cutaway: http://www.ulalaunch.com/site/docs/products/Cutaways/Atlas500_Cutaway.pdf
Spaceflight 101 Atlas V-541 page: http://www.spaceflight101.com/atlas-v-541.html
MAJOR MILITARY/GOVERNMENT SPACE RESOURCES:
National Reconnaissance Office (NRO): http://www.nro.gov/
Patrick AFB (45th Space Wing) (Cape Canaveral): http://www.patrick.af.mil/
5th Space Launch Squadron (5th SLS):
Vandenberg AFB (30th Space Wing): http://www.vandenberg.af.mil/
4th Space Launch Squadron (4th SLS):
Air Force Space Command: http://www.afspc.af.mil/
Peterson AFB (21st Space Wing): http://www.peterson.af.mil/