NanoSail-D2

NanoSail-D2

Mission type	Technology
Operator	NASA
Mission duration	240 days
Spacecraft properties
Spacecraft type	3U CubeSat
Launch mass	4 kilograms (8.8 lb)
Start of mission
Launch date	20 November 2010, 01:25 (2010-11-20UTC01:25Z) UTC
Rocket	Minotaur IV/HAPS
Launch site	Kodiak Pad 1
Contractor	Orbital Sciences
Deployed from	FASTSAT
Deployment date	Commanded: 3 December 2010 Occurred: 17 January 2011
End of mission
Decay date	17 September 2011
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Perigee	654 kilometers (406 mi)
Apogee	623 kilometers (387 mi)
Inclination	71.9761 degrees
Period	97.45 minutes

NanoSail-D2 was a small satellite built by NASA's Marshall Space Flight Center and Ames Research Center to study the deployment of a solar sail in space. It was a three-unit CubeSat, measuring 30×10×10 centimetres (11.8×3.9×3.9 in) with a mass of 4 kilograms (8.8 lb). Its solar sail had an area of 10 square meters (110 sq ft), and was deployed in around five seconds.

It was planned to be deployed from the FASTSAT satellite around 3 December 2010, two weeks after launch. The satellite did not eject at that time, but on January 17, 2011, it ejected on its own and deployed its sail three days later on the 20th. The beacon signal began transmitting after ejection and was first received on the afternoon of January 19, 2011.

Chronology

NanoSail-D2 was originally built as a ground spare for the NanoSail-D satellite, which was launched aboard a Falcon 1 in 2008, and was subsequently lost when the rocket malfunctioned during stage separation. Over the next two years improvements were made to the spare, and the satellite was incorporated into the FASTSAT mission.

NanoSail-D2 was launched aboard a Minotaur IV/HAPS rocket, inside the FASTSAT satellite. FASTSAT was a secondary payload on the launch, with the primary payload being STPSat-2. The launch also carried RAX, O/OREOS, FalconSat-5, and the two FASTRAC satellites; Sara-Lily and Emma. The Minotaur was launched from Launch Pad 1 of the Kodiak Launch Complex at 01:25 UTC on 20 November 2010. Orbital Sciences Corporation conducted the launch under a contract with the United States Air Force.

FASTSAT was deployed into a low Earth orbit with a circular orbit of 650 kilometers (400 mi) of altitude and 72 degrees of inclination. NanoSail-D2 was expected to separate from FASTSAT on December 6, but although the bay door opened ejection did not occur. Successful ejection was confirmed on 19 January 2011; it is unclear what caused the ejection mechanism to fail and then ultimately release at this later date. NASA requested amateur radio operators listen for the beacon signal from NanoSail-D. They did and picked up the 1-second beacon transmissions which were transmitted every 10 seconds. While battery power was soon exhausted, as predicted by the principal investigator, Dean Alhorn, the spacecraft was expected to sail on in low-Earth orbit for 70 to 120 days, depending on atmospheric conditions, before it burnt up, and to become easier to view after the atmosphere stabilized its tumbling.

To generate publicity and to encourage observations while the sail was still in orbit, NASA and Spaceweather.com announced a photography competition with a grand prize of $500 to capture images of the solar sail in orbit.

On September 17, 2011, the solar sail re-entered the atmosphere after 240 days in orbit, though this was only announced on November 29, 2011.

External links

• NASA NanoSail-D Mission page
• NanoSail-D dashboard
• Twitter page
• An index of images by astrophotographer Ralf Vandebergh created with a telescope mounted camera.
• information about NanoSail-D2 on eoportal.org