ROCKOT - The proven, competitive launch system for small satellites

2000 ◽  
Author(s):  
P. Freeborn ◽  
G. Stamerjohanns ◽  
M. Kinnersley
Keyword(s):  
Small Satellites

Small Satellites: Past, Present, and Future

2009 ◽  
Author(s):  
H. Helvajian ◽  
S. Janson
Keyword(s):  
Small Satellites

Design and demonstration of a micro air-fed magnetoplasmadynamic thruster for small satellites

2021 ◽  
Vol 181 ◽  
pp. 482-491
Author(s):  
Zihao Wang ◽  
Youngho Eun ◽  
Xiaofeng Wu
Keyword(s):  
Small Satellites

A Novel Approach for Pivot-based Sensor Fusion of Small Satellites

2021 ◽  
Vol 45 ◽  
pp. 101261
Author(s):  
Ngoc V.B. Pham ◽  
Tu N. Nguyen ◽  
Tan D. Ngo ◽  
Anh T. Truong ◽  
Giang L. Nguyen
Keyword(s):  
Sensor Fusion ◽  
Small Satellites ◽  
Novel Approach

scholarly journals Design of a high-stability heterogeneous clock system for small satellites in LEO

GPS Solutions ◽  
2021 ◽  
Vol 25 (3) ◽  
Author(s):  
Damon Van Buren ◽  
Penina Axelrad ◽  
Scott Palo
Keyword(s):  
Low Power ◽  
High Stability ◽  
Time Frame ◽  
System Stability ◽  
Small Satellite ◽  
Crystal Oscillator ◽  
Small Satellites ◽  
Clock System ◽  
Wide Range

AbstractWe describe our investigation into the performance of low-power heterogeneous timing systems for small satellites, using real GPS observables from the GRACE Follow-On mission. Small satellites have become capable platforms for a wide range of commercial, scientific and defense missions, but they are still unable to meet the needs of missions that require precise timing, on the order of a few nanoseconds. Improved low-power onboard clocks would make small satellites a viable option for even more missions, enabling radio aperture interferometry, improved radio occultation measurements, high altitude GPS navigation, and GPS augmentation missions, among others. One approach for providing improved small satellite timekeeping is to combine a heterogeneous group of oscillators, each of which provides the best stability over a different time frame. A hardware architecture that uses a single-crystal oscillator, one or more Chip Scale Atomic Clocks (CSACs) and the reference time from a GPS receiver is presented. The clocks each contribute stability over a subset of timeframes, resulting in excellent overall system stability for timeframes ranging from less than a second to several days. A Kalman filter is used to estimate the long-term errors of the CSACs based on the CSAC-GPS time difference, and the improved CSAC time is used to discipline the crystal oscillator, which provides the high-stability reference clock for the small satellite. Simulations using GRACE-FO observations show time error standard deviations for the system range from 2.3 ns down to 1.3 ns for the clock system, depending on how many CSACs are used. The results provide insight into the timing performance which could be achieved on small LEO spacecraft by a low power timing system.

scholarly journals Digital Manufacturing for Smart Small Satellites Systems

2021 ◽  
Vol 180 ◽  
pp. 150-161
Author(s):  
Markus Krauß ◽  
Florian Leutert ◽  
Markus R. Scholz ◽  
Michael Fritscher ◽  
Robin Heß ◽  
...  
Keyword(s):  
Digital Manufacturing ◽  
Small Satellites

scholarly journals Modeling of onboard systems operation of small satellites based on general logical-probabilistic method

2021 ◽  
Vol 1745 (1) ◽  
pp. 012086
Author(s):  
V V Salmin ◽  
I S Tkachenko ◽  
S S Volgin ◽  
M A Ivanushkin
Keyword(s):  
Probabilistic Method ◽  
Small Satellites
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