Home Space Economy NASA State of the Art Report: Small Spacecraft Technology (NASA 2024)

NASA State of the Art Report: Small Spacecraft Technology (NASA 2024)

Synopsis

The report provides an overview of current technologies and development status for various small spacecraft subsystems, with a focus on components and systems that have achieved Technology Readiness Level (TRL) 5 or higher.

Power Systems

  • Solar cells: Multi-junction III-V semiconductor solar cells with efficiencies over 32% are state-of-the-art. Triple junction cells offer a good efficiency/cost ratio.
  • Solar panels: Rigid deployable and body mounted panels available. Specific power up to 165 W/kg. Peak power ranges from 2W (1U face) to 179W.
  • Batteries: Lithium-ion and lithium polymer secondary batteries widely used. Energy densities up to 265 Wh/kg. Carbon-based anodes can provide fast charging and high cycle life.
  • Power management: Modular electronic power systems with peak power tracking, battery charging, voltage regulation. Power ranges from 1-500W.

Propulsion

  • Chemical thrusters with green propellants, microresistojet thrusters, pulsed plasma thrusters, and water electrolysis thrusters discussed.
  • Electric propulsion options cover Hall effect thrusters, ion engines, pulsed inductive thrusters and more.
  • Propellantless systems like electrodynamic tethers and solar sails also overviewed.

Guidance, Navigation and Control

  • COTS star trackers, sun sensors, IMUs, magnetometers commonly used.
  • Reaction/momentum wheels and control moment gyros from 0.04-45 Nms capability.
  • Thrusters (chemical and electric) also used for attitude control.

Structures, Materials and Mechanisms

  • Materials like aluminum, titanium, polymers, and composites used.
  • Deployment mechanisms using shape memory alloys, Frangibolts.
  • Structural performance from femto/picosats to ESPA-class smallsats covered.

Thermal Control

  • Multi-layer insulation, optical coatings, heaters, heat pipes, loop heat pipes, thermal straps.
  • Active systems use electrical heaters, thermoelectric coolers, and fluid loops.

Avionics

  • On-board computers with processors from ARM Cortex-M0 to M7, PowerPC, LEON3-FT and RAD750.
  • FPGAs from Xilinx, Microsemi and Intel (formerly Altera).
  • Memory options include MRAM, FRAM, NAND/NOR flash, SD/microSD cards.

Communications

  • S-band transmitters and transceivers available at all power levels and data rates.
  • X-band becoming more popular for high data rate needs.
  • Optical comm with data rates over 200 Mbps demonstrated on orbit.

The report covers additional subsystems like software, ground systems, launch and deployment, tracking, and deorbit systems. It provides a good overview of the current state of small spacecraft technologies.

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