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FRETS1 SATELLITE Presented at HPARC, 2012-02-08

FRETS1 Satellite

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FRETS1 satellite project, including a custom ion engine, presented to the Hazel Park Amateur Radio Club (HPARC) on 2012-02-08.

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FRETS1 SATELLITE

Presented at HPARC, 2012-02-08

Agenda

Mission

Concept of Operations

Technology

Amateur Radio Tie-Ins

Mission - Goals

Test a new ion engine design

Electrostatic principles

Pulsed plasma generation

Exhaust flow beyond classic Child-Langmuir limit

Increased thrust per [kg, m3]

(future) Alternative plasma generation method

Lower power requirements

(new) Alternative fuel storage

Lower complexity for gas-based thrusters

Mission – TubeSat Standard

Images: Interorbital Systems

500 grams + 250 grams payload

127mm

tall

Mission – TubeSat Orbit

310 km polar sun-synchronous orbit

Decaying, 3-12 weeks

90.7 minute orbit period

Launch by

Interorbital Systems

interorbital.com

Image: Interorbital Systems

Mission - Thermal

Average temperature, °CPCB Material Metal Strips Hot Case Cold Case

Green PCB Aluminum, polished 95 -7

Green PCB Aluminum, anodized 68 -18

White PCB Polished copper 89 -7

White PCB Carbon black paint 84 1

White PCB Aluminum, polished 84 -19

White PCB 3M Black Velvet paint 83 1

White PCB Anodized black metal 81 -1

White PCB Gray paint 77 -6

White PCB Aluminum, anodized 57 -28

ConOps – Launch Operations

Wait

Launch

Coast

Release

Wake

Initialize

ConOps – Orbit Operations

Safe

Engine baseline experiments

Engine effect experiments

Sensor experiments

Mechanical experiments

Energy gathering

Communication relay

Status reporting

ConOps – End of Mission Ops

Orbit decay

Reentry

Technology - Communications

MX614

AX25

Encoder

PIC

AX25

Decoder

PIC Transceiver

433MHz band

100mW

Radiometrix

Amplifier

500mW

Radiometrix

Main

CPU

BasicX 24

Technology – Comm. Board

Technology - Solar

48 solar cells

8 strips of 6

Technology - Solar

Radial

0.75 Watt avg.

on sun side

Flat/Bullet

0.75 Watt avg.

on sun side

Sun Seeker

1.18 Watt avg.

on sun side

Technology - Power

Voltage

Regulator

Li-Ion

Battery

3.7V

5200mAh

8 Current

Sensors

Deployment

Switches

Step-Up

Voltage

Converter

CPU

Board

Comm.

Board

Engine

Board

8 Channel

ADC

4.2V5.7V

Diodes

SPI

Technology - Microprocessor

BasicX-24

I2C interface

IMU

Flash memory

SPI Solar ADC

Images: http://basicx.com/

Technology - Microprocessor

SEU current sensor

Shielding?

Image: http://www.aero.org/publications/crosslink/winter2000/03.html

Technology - Engine

Electrostatic

Child-Langmuir limit

to fuel flow

Fuel flow limit

to Thrust density

Use lasers to get

past classic limits

Low thrust confuses

sensors

Technology - Fuel

Nitrous oxide cylinder

Lots of fuel

Not ConOps friendly

Closed cell foam

Easy storage – ConOps

Semi-untested in space

Pulsed Plasma Thruster

Wide variety of fuel species

Energy intensive Overview of PPT operation. (1) Energy

storage unit. (2) Ignitor. (3) Fuel rod.

(4) Plasma acceleration Credit: NASAImages: http://www.lelandltd.com/mini_cartridges.htm

http://www.nasa.gov/centers/glenn/about/fs23grc.html

Technology – Attitude Sensing

9 DOF

HMC5883L magnetometer

ADXL345 accelerometer

ITG-3200 gyro

I2C interface

1.0 gram

Manual correction for

drift and noise required.

http://www.sparkfun.com/products/10183

Technology – Attitude Sensing

9 DOF & Temperature

Kalman filter

1.3 grams

45mA @ 5V

0.225 W

http://tech.yostengineering.com/3-space-sensor/product-family/embedded

Open question:

Will Kalman filter out

our engine’s effects?

Technology – Attitude Control

Active Magnetorquer

High Power

High Price

Image: ISIS Magnetorqer, http://www.cubesatshop.com

Technology – Attitude Control

Passive magnetic attitude control

Permanent magnet

Hysteresis rods

Images: http://www-personal.umich.edu/~mjregan/MCubed/Pages/O&C.html

http://cosmiac.ece.unm.edu

- Slow convergence

- Large fraction of payload space for rods

Technology – Attitude Control

Piezoelectric Energy Harvesting

Kinetic and spring energy to electrical energy

Images: http://piezo.com/prodproto4EHkit.html

- New approach

- Dampens vibration

- Dampens rotational acceleration using lever arms

Amateur Radio Tie-Ins

Store and forward message(s)

Compressed Sensing telemetry

AX.25 Relays

Other ideas?!

FRETS1 Satellite

frets1.com

Wes Faler

[email protected] Smith