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admin | Category: Modular Container Homes | 30.01.2015
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While in theory both types of satellite can be launched from either Vandenberg or Cape Canaveral, most NOSS launches have occurred from Vandenberg – for current-generation spacecraft the only exceptions have been NROL-23 and NROL-30, both launched by rockets that did not have launch facilities available at Vandenberg.
The payload fairing encapsulating the NROL-36 payload is a four-metre (13-foot) Extended Payload Fairing (EPF), which is 13.1 metres (43 feet) in length. Based on the information that is available, it is likely that NROL-36 will be a pair of NOSS satellites, however this is not certain. Current-generation NOSS satellites are launched and operated in pairs, which orbit the Earth in close proximity to each other. The first launch of third-generation satellites occurred in September 2001, using an Atlas IIAS. The US Strategic Command Satellite Catalog lists the second satellite in each pair as being debris from the first, unlike with previous-generation spacecraft where it lists each spacecraft as a separate satellite. NROL-36 will be the sixth third-generation launch, following NROL-13 and 18, NROL-23 was launched by the last Atlas IIIB in 2005, NROL-30 was launched by an Atlas V 401 in 2007, and NROL-34 was launched by an Atlas V 411 last year. The NROL-30 launch was a partial failure, with the Centaur’s second burn ending four seconds prematurely as the result of a propellant leak caused by a faulty valve.
It was initially speculated that NROL-34 launching on the more powerful 411 configuration was to eliminate the need for the second burn, however with NROL-36 reverting to the 401, the reason for changing the configuration remains unclear. The Atlas V which will launch NROL-36 has the tail number AV-033, and has been named Rosie. This configuration consists of a Common Core Booster first stage, with a single-engined Centaur upper stage, and a four-metre payload fairing. Stage separation will occur six seconds after first stage cutoff, with the Centaur’s RL10 engine igniting ten seconds later. Once this is complete, the Centaur will enter an extended coast phase, lasting around an hour, before a second burn lasting around a minute to reach the NOSS deployment orbit. Normally following spacecraft separation, the Centaur would be disposed of through either pacification, deorbiting, or ejection from Earth orbit; however AV-033 will instead continue to deploy eleven CubeSats in a test of a new extended mission kit which is flying for the first time on this flight.
It is anticipated that in order to manoeuvre from the NOSS deployment orbit to the published orbit into which the CubeSats will be deployed, the Centaur will have to make two additional burns to lower its orbit. The CubeSat payload is designated Operationally Unique Technique Satellite, or OUTSat, and consists of eight PPOD dispensers attached to the aft end of the Centaur via an Aft Bulkhead Carrier (ABC), which is being used for the first time on this mission. Four of the CubeSats are being launched as part of NASA’s Educational Launch of Nanosatellites (ELaNa) programme.
ELaNa II was cancelled, having originally scheduled to accompany an Operationally Responsive Space payload into orbit, while ELaNa IV and V are manifested for launches next year on Minotaur I and Falcon 9 rockets respectively. The satellites which are being launched as part of ELaNa VI are CINEMA 1, for a multinational research consortium, CSSWE for the University of Colorado at Boulder, CXBN for Morehead State University, and CP5 for the California Polytechnic University.
The CubeSat for Ion, Neutral, Electron and Magnetic fields, or CINEMA 1, is a three-unit CubeSat built and operated by a consortium led by the University of California at Berkeley, and including Imperial College London, Kyung Hee University, and NASA’s Ames Research Center.

Colorado Student Space Weather Experiment, or CSSWE, is another three-unit satellite which will be used to study electron and proton flux in the magnetosphere, as part of an investigation to determine how these fluxes are affected by solar flares. Space-Based Telescopes for Actionable Refinement of Ephemeris A, or STARE-A, also known as Re, is also a three-unit CubeSat based on the Boeing-built Colony II bus, and is intended to study optical tracking of space debris. Rosie will be launched from Space Launch Complex 3E (SLC-3E) at the Vandenberg Air Force Base in California. SLC-3E was initially used for Atlas-Agena launches, after which three Atlas SLV-3s made suborbital launches with X-23A PRIME spacecraft, and an Atlas SLV-3 failed to orbit twelve payloads in a single launch.
Between 1992 and 1996 the complex was redeveloped to accommodate the Atlas II, with the first of three launches occurring in 1999 with the Terra satellite, following two years of delays. The Atlas V made its first launch from SLC-3E in March 2008, carrying an Improved Trumpet satellite, NROL-28. The Atlas V is operated by United Launch Alliance, a corporation formed in 2006 to provide launch services to the US Government. Your requested content delivery powered by FeedBlitz, LLC, 9 Thoreau Way, Sudbury, MA 01776, USA.
The rocket is believed to be carrying a pair of ocean surveillance satellites to locate ships at sea, in a mission designated NROL-36. USA-144, the second Misty satellite, was also launched into a 63.4 degree orbit, however since Misty is believed to be derived from the KH-11 imaging satellite, a Delta IV Heavy would be needed to launch it.
Originally developed for the Atlas II, it is the second-largest of the three four-metre fairings used on the Atlas V, being 90 centimetres longer than the Long Payload Fairing, and 90 centimetres shorter than the Extra-Extended Payload Fairing.
Alternatively it could be a one-off mission, part of a new series of spacecraft, or a modified Trumpet or SDS; however these possibilities are all very unlikely.
Earlier spacecraft operated in groups of three, nicknamed Triads, and also included a separate dispenser to manoeuvre to their operational orbit, and deploy the three satellites.
The MSD, or Multiple Satellite Dispenser, is believed to have been powered by an FW-4D motor, and acted both as an upper stage and a dispenser for the four satellites. Designated NROL-13 or USA-160, the payload consisted of two satellites, leading to speculation that a third spacecraft had failed to separate. This resulted in a lower orbit than had been planned, however the spacecraft were able to raise themselves to their operational altitude.
A Russian-built RD-180 engine powers the Common Core Booster, while the Centaur is powered by a US-built RL10-A-4 engine.
Around 15 seconds later, the payload fairing will separate, at which point official updates on the status of the launch will be discontinued. Two minutes later, the two NOSS spacecraft will separate from the Centaur; initially remaining attached to each other, and the Centaur will perform a collision avoidance manoeuvre. Following these burns, the CubeSats are expected to separate around three hours after launch. The ABC is attached to a point on the Centaur where a Helium tank would normally be located.
It is the first of three satellites to be launched for the consortium which will study the Earth’s magnetosphere. Cosmic X-Ray Background, or CXBN, is a two-unit CubeSat which will study cosmic background x-rays.

SMDC-ONE, or Space Missile Defense Command Operational Nanosatellite Effect, is an experimental communications programme intended to transmit data packets and real-time radio messages. It carries two demonstration payloads; one will use a 50 centimetre (20 inch) mesh antenna to track electronic tags on shipping containers, whilst the second will demonstrate a new flight processor.
The pad was originally part of the Point Arguello Naval Air Station, and designated Launch Complex 1-2, supporting its first launch in July 1961 when an Atlas-Agena launched MIDAS-3. This was followed by the launch of a DMSP weather satellite in October 2009, and an FIA Radar satellite, NROL-41, in September 2010. ULA also operates the Delta II and Delta IV carrier rockets, and NROL-36 is their seventh launch of the year with four more planned.
The next launch is expected to occur later this month, when an Atlas V 401 will deploy NASA’s Radiation Belt Storm Probes in a launch from Cape Canaveral. In addition to the classified spacecraft, eleven CubeSats will be deployed as secondary payloads. The EPF has previously been used on launches carrying NOSS and Improved Trumpet satellites, while SDS launches use the Long Payload Fairing.
The December 2003 launch of NROL-18, or USA-173, showed that the new satellites were instead launched in pairs. The first stage burn will last around four minutes and three seconds, with the RD-180 engine being throttled back to limit acceleration three seconds before cutoff. Assuming the Centaur is performing a two-burn insertion, its first burn will last about 14 minutes and 27 seconds. It is unclear what action will be taken to dispose of the Centaur following the deployment of the CubeSats; however the absence of a NOTAM suggests that it will not be deorbited. This tank is not required on missions using the extended mission kit, as the other helium tanks have been enlarged.
CP5 is a single-unit satellite which will be used to study the use of a thin film to deorbit the satellite by increasing its drag. The most recent launch occurred in March 2011, with the deployment of NROL-34, a pair of NOSS satellites like those expected to be deployed by AV-033. The next scheduled NRO launch is planned for next year, when a Delta IV Heavy will launch NROL-65 from Vandenberg.
Second generation spacecraft were deployed by an SLDCOM, or Satellite Launch Dispenser Communications, spacecraft. The next launch scheduled to occur from the pad will be of the Landsat Data Continuity Mission next February.
Following deployment of the NOSS satellites, the SLDCOM would raise itself into a higher orbit for use as a communications satellite. As such, these products will reflect a higher Shipping Weight compared to the unprotected product. It is rumoured that the Interim Control Module developed for the International Space Station in the event of the Zvezda module’s failure was based on SLDCOM, and built from spare parts.

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