Interplanetary CubeSats: Opening the Solar System to a Broad Community at Lower Cost
Project Introduction
Today, Solar System exploration missions are the exclusive domain of space agencies and their scientists and engineers who can muster multi-hundred-million dollar budgets. While their accomplishments are broad, highly sophisticated and literally out of this world, the high cost limits our pace of important discoveries. Interplanetary CubeSats offer an opportunity to conduct focused science investigations around the inner Solar System at a cost ten times lower than missions mounted today. In much the same way that CubeSats weighing a few pounds have dramatically increased low cost access to space experimentation in low Earth orbit, this study intends to focus development of six technologies in unison so as to enable dramatically lower cost exploration of the Solar System and our Earth's more distant environs. Using the pressure of sunlight, a gravitationally defined Interplanetary Superhighway, advanced electronics and instrumentation, and laser communications, may extend the turn-of-the-millennium CubeSat standard for nanosatellites to distances far beyond Earth's magnetic cocoon. CubeSats in low Earth orbit have enabled dozens of universities to develop and place in orbit student-led, student-designed, student-built, and student-operated satellites investigating all manner of scientifically exciting phenomena, while giving graduates of these programs a competitive edge they bring to American technology and industry. Additionally, CubeSats have enabled Government-sponsored space experimentation and technology development on an accelerated schedule for unprecedented low cost. If successful, this system study of the technologies to enable Interplanetary CubeSats will open the door to a similar revolution in access to space and new discoveries beyond Earth.
More »Anticipated Benefits
A. A useful interplanetary s/c at 10 kg is dramatically lighter than any previous, enabling utilization of excess payload capacity to GEO and beyond to produce additional science and exploration results.#B. Order-of-magnitude reduction in cost of very focused exploration missions beyond Earth.#C. Combining A & B makes more missions to more destinations possible, moving Solar System exploration from a few missions per decade to a few missions per year.#D. Opens beyond-Earth destinations to advanced elements of the CubeSat community, including hands-on education of college- and graduate-level students.#E. Optical telecom of small mass, size, power and cost will be valuable to other missions. May allow reduction of costs from traditional rf and DSN utilization.#F. Introduces solar sail application to other NASA missions, permitting unprecedented maneuvering for very small s/c at low cost; provides deltaV of 5-20+ m/sec/day without propellant, enabling inexpensive transport to and among multiple destinations
More »Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Jet Propulsion Laboratory
(JPL)
|
Lead Organization | NASA Center | Pasadena, California |
| California Polytechnic State University-San Luis Obispo (Cal Poly) | Supporting Organization | Academia | San Luis Obispo, California |
| Stellar Exploration, Inc. | Supporting Organization | Industry | San Luis Obispo, California |
| The Planetary Society | Supporting Organization | Non-Profit Institution |
Primary U.S. Work Locations
-
California
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Jet Propulsion Laboratory (JPL)
Responsible Program:
- NASA Innovative Advanced Concepts
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Technology Maturity (TRL)
| Start: | 2 |
| Current: | 3 |
| Estimated End: | 3 |
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.2 Electric Space Propulsion
- TX01.2.2 Electrostatic
Target Destination
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