Official name PODSAT
Alternative name PODSAT
Cospar ID 2018-023B
Norad ID 43229
Launch date 2018-03-06
Launch site AFETR
Launch vehicle Falcon-9 v1.2
Country/Organization USA
Type application Technology
Operator DARPA
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 181.82
Inclination (deg) 26.83
Perigee (km) 202
Apogee (km) 8305
Eccentricity 0.95250969789585
Mean motion (revs. per day) 7.91992080079199
Semi-Major axis (km) 10631.635
Raan (deg) 239.1083
Arg of perigee (deg) 159.3148
Shape Box
Mass (kg) 90
Height (m) 0.3
Width (m) 0.3
Depth (m) 0.3
Span (m^2) 0.3
Lifetime < 1 year
Contractors NovaWurks (satlets), SSL (POD chassis)
Propulsion ?
Configuration POD chassis with 4 aggregated HiSat satlets
Power Solar cells, batteries

PODSAT 1 (Payload Orbital Delivery Satellite) is the second DARPA-sponsored mission by NovaWurks to demonstrate the satlets technology.

Satlets are a new low-cost, modular satellite architecture that can scale almost infinitely. Satlets are small modules that incorporate multiple essential satellite functions and share data, power and thermal management capabilities. Satlets physically aggregate in different combinations that would provide capabilities to accomplish diverse missions.

The Payload Orbital Delivery system Satellite (PODSat) is a four-HISat PAC itegrated with a POD chassis nearing the start of assembly, integration, and test. PODSat was integrated with the SSL built Hispasat 30W-6 satellite. PODSat is designed to be the free-flying element of the DARPA-funded Hosted POD Assembly (HPA), which seeks to provide a platform (the POD) and a separation mechanism for it be deployed by a host spacecraft. Conceived to take advantage of under-utilized launch vehicle payload mass and reliable, frequent launch opportunities, the initial HPA would be hosted on a geostationary communications satellite, with the PODSat deployment occurring in a subsynchronous geostationary transfer orbit.

PODSat would provide a demonstration of the ability of cellular architecture to incorporate a structural element, the POD chassis, into a PAC. Similar to the way app-based software architectures allow easy integration of new software, celluar architectures could offer that same feature to a variety of hardware options.

The PODSat experiment would also provide valuable in-orbit data on an orbit environmental regime outside of the first two experiments.

Satellite COSPAR Date LS Launch Vehicle Remarks
PODSAT 2018-023B 2018-03-06 AFETR Falcon-9 v1.2 with Hispasat 30W-6 (Hispasat 1F)