TacSat-4

TacSat-4

Computer model of TacSat-4
Names	JSW 1 COMMx Tactical Microsatellite Innovative Naval Prototype (INP)
Mission type	Technology, Communications
Operator	Naval Research Laboratory (NRL) Applied Physics Laboratory (APL) Air Force Research Laboratory (AFRL)
COSPAR ID	2011-052A
SATCAT no.	37818
Mission duration	2 years (planned)
Spacecraft properties
Spacecraft	TacSat-4
Spacecraft type	TacSat
Bus	JSW bus
Manufacturer	Naval Research Laboratory (bus and payload) Applied Physics Laboratory (bus)
Launch mass	468 kg (1,032 lb)
Power	1 kW
Start of mission
Launch date	27 September 2011, 15:49:00 UTC
Rocket	Minotaur IV+
Launch site	Kodiak Launch Complex, LP-1
Contractor	Orbital Sciences Corporation (OSC)
Orbital parameters
Reference system	Geocentric orbit
Regime	Low Earth orbit
Perigee altitude	472 km (293 mi)
Apogee altitude	12,291 km (7,637 mi)
Inclination	63.1°
Period	238.9 minutes
TacSat series ← TacSat-3 TacSat-6 →

TacSat-4 is the third in a series of U.S. military experimental technology and communication satellites. The United States Naval Research Laboratory (NRL) is the program manager. The Office of Naval Research (ONR) sponsored the development of the payload and funded the first year of operations. The Office of the Director of Defense Research and Engineering (DDR&E) funded the standardized spacecraft bus and the Operationally Responsive Space Office (ORS) funded the launch that will be performed by the Air Force's Space and Missile Systems Center (SMC).

The spacecraft was completed by the end of 2009, and was launched on 27 September 2011, at 14:49:00 UTC, on a Minotaur IV launch vehicle into a highly elliptical orbit (HEO).^[1][2][3][4]

TacSat-4 is equipped with a 3.6 m (12 ft) antenna operating 10 Ultra High Frequency (UHF) channels that can be used for any combination of communications, data ex-filtration or Blue Force Tracking (BFT). TacSat-4 will fly the highly elliptical, 4-hour, orbit (12,050 kilometers at peak) providing typical payload communication periods of two hours per orbit. TacSat-4's orbit also allows it to cover the high latitudes.

Part of its capability is rapid (within 24 hours) reallocation to different theaters worldwide, in support of unexpected operations. Command and control of TacSat-4 will be performed at the United States Naval Research Laboratory (NRL) Satellite Operations Center at Blossom Point, Maryland. Payload tasking will be performed via the SIPRNet based Virtual Mission Operations Center (VMOC).

All TacSat satellites are designed to demonstrate the ability to provide real-time data collected from space to combatant commanders in the field.^[5]

The spacecraft bus was built by NRL and Johns Hopkins University Applied Physics Laboratory (APL) to mature ORS bus standards developed by an Integrated (government and industry) System Engineering Team, the "ISET Team", with active representation from AeroAstro, Air Force Research Laboratory, Johns Hopkins University Applied Physics Laboratory, ATK Space, Ball Aerospace & Technologies, Boeing, Design Net Engineering, General Dynamics AIS, Microcosm, Sierra Nevada Corp., Massachusetts Institute of Technology, Lincoln Laboratory, Orbital Sciences Corporation, NRL, SMC, Space Systems/Loral, and Raytheon. Lithium-ion battery power provided by Quallion.

• TacSat-4 (Tactical Satellite-4), eoPortal, on the eo "Sharing Earth Observation Resources" website