AMSAT Fox Series Launch Schedule Update

The launches of AMSAT satellites Fox-1Cliff and Fox-1D have been rebooked from the original Spaceflight Formosat-5/Sherpa mission aboard a SpaceX Falcon 9  on to two separate new launches.

Fox-1D will now ride to orbit on an Indian PSLV vehicle scheduled to launch from Satish Dhawan Space Centre in Sriharikota, India in late 2017.

Fox-1Cliff will launch on Spaceflight’s SSO-A dedicated rideshare mission aboard a SpaceX Falcon 9 scheduled to launch from Vandenberg Air Force Base in California in late 2017 or early 2018.

These moves will serve to expedite the launch of these two satellites, both of which carry an amateur radio U/v FM repeater and an experimental L/v FM repeater.  The satellites also carry scientific experiments, from university partners Penn State, Vanderbilt University ISDE, Virginia Tech, and University of Iowa.

In addition to the launch of Fox-1Cliff and Fox-1D, AMSAT is awaiting the launches of RadFxSat and RadFxSat-2. RadFxSat is currently manifested for launch on August 29, 2017 aboard the ELaNa XIV mission, as a secondary payload with the Joint Polar Satellite System (JPSS)-1 on a Delta II from Vandenberg Air Force Base, California. RadFxSat-2 will be launched by Virgin Galactic on their LauncherOne air launch system from Mojave, CA on the ELaNa XX mission no earlier than December 2017.

 

Two projects with AMSAT ties selected for NASA launches

Two cubesat missions with ties to AMSAT have been selected as part of the eighth round of the NASA CubeSat Launch Initiative. These spacecraft are eligible for placement on a launch manifest after final negotiations, depending on the availability of a flight opportunity.

TJREVERB is a cubesat from Thomas Jefferson High School for Science and Technology, in Alexandria, Virginia. This satellite will include an AMSAT Fox mode U/v FM radio system, and will be capable of serving as an analog FM repeater.

HuskySat-1 from the University of Washington in Seattle will carry a mode V/u linear transponder and 1200 baud BPSK beacon similar to RadFXsat-2. The satellite will demonstrate plasma propulsion and high gain telemetry in advance of a larger cubesat lunar mission.

The complete list of satellites selected may be found at on the NASA web page. Further information will be shared when available.

RadFXsat-2 receives IARU frequency coordination

RadFXSat-2 is a 1U cubesat technology demonstration mission from Vanderbilt University that has been accepted for launch as part of NASA’s CubeSat Launch Initiative. Vanderbilt University is partnered with AMSAT, who will provide the satellite and communications for the experiments onboard as part of the AMSAT Fox program.

AMSAT recently received IARU frequency coordination for a 1200 baud BPSK telemetry downlink beacon on 435.750 MHz, and a mode V/u inverting transponder with an uplink of 145.860-145.890 MHz and a downlink of 435.760-435.790 MHz.

RadFXSat-2 is currently manifested as part of the ELaNA XX mission, scheduled for no earlier than December 2017, on a Virgin Galactic Launcher One, from Mojave, California. Other satellites on the mission include:

  • CACTUS-1 – Capitol Technology University, Laurel, Md.
  • ALBus – NASA Glenn Research Center, Cleveland, Ohio
  • SurfSat – University of Central Florida, Orlando, Fla.
  • Q-PACE – University of Central Florida, Orlando, Fla.
  • CAPE-3 – University of Louisiana Lafayette, La.
  • MiTEE – University of Michigan, Ann Arbor, Mich.
  • PICS – Brigham Young University, Provo, Utah
  • INCA – New Mexico State University, Las Cruces, N.M.
  • MicroMas-2b – Massachusetts Institute of Technology, Lexington, Mass.
  • EXOCUBE – California Polytechnic University, San Louis Obispo, Calif.
  • PolarCube – University of Colorado at Boulder, Boulder, Colo.

AO-7 eclipses return, satellite now primarily in Mode U/v

From AMSAT-bb (http://amsat.org/pipermail/amsat-bb/2016-November/061297.html):

The AMSAT satellite status page at http://www.amsat.org/status/ indicates
that as of the morning of 11/25/2016, AO-7 is once again entering eclipse
each orbit. This means that the 24 Hour mode change timer is interrupted
each orbit, and the satellite will be found primarily in Mode U/v (aka Mode
B).

As the satellite is powered solely by the now 42 year-old solar panels, it
is very sensitive to strong uplink signals, particularly CW. Users should
closely monitor their downlink for excessive chirp, warbling or “FM’ing” and
reduce power as necessary. More information including frequencies can be
found at http://ww2.amsat.org/?page_id=1031

73, Drew KO4MA

AMSAT VP Operations