CansatLeader Training Program ReportsCansatLeader Training Program Reports December 12, 2011 The...

Cansat Leader Training Program Reports

December 12, 2011

The 3rd Nano-Satellite Symposium

What is Cansat Leader Training Program?

Established in 2010 to contribute to capacity building in space technology and improve teaching methods-based space engineering education

CLTP provides a training course to experience whole cycle of CanSat development that involves design, fabrication and launch by a model rocket or a

captive balloon lectures on space engineering and nano-satellite

development The participants will be expected to make a textbook in

their own language for preparing education in their home countries.

CLTP is opened for researchers and educators who wish to learn the hands-on space engineering education methods using Cansat.

The 1st CLTP was held in Wakayama University from February 14th to March 20th, 2011.

CLTP2 was held from 14th November to 9th December at Nihon University in Funabashi city (about 40minutes from Tokyo by train).

Ten researchers participated in CLTP2 from 10 countries. They formed 4 teams.

UNISEC and Nihon University students organized the program. The students supported the participants making the Cansats and conducting

the balloon experiments and rocket launch. CLTP2 is a good experience for students, too.

Wakayama University and Mr. Kosada (Young Astronaut Club Japan) helped the launch of model rocket.

Thu TrongVu

(Vietnam)

BatmuunkhEnkhbat

(Mongolia)

SawatTantiphanwadi

(Thailand)

Osman Ceylan

(Turkey)

OgechukwuStanislaus

Nnadih(Nigeria)

Manfred Quarshie(Ghana)

AgfiantoEko Putra

(Indonesia)

SyahrimAzhanIbrahim

(Malaysia)

2nd Cansat Leader Training Program (CLTP2)

Renato Miyagusuku

Rios(Peru)

Ling Keck Voon

(Singapore)

Team A Team B Team C Team D

Schedule of CLTP2

Period ContentsBefore CLTP2 Homework on electric circuit design and fabrication of a small electric board

First week Opening ceremony Briefing on CLTP2 (15th Nov) Lectures on nanosatellite design, systems engineering, and capacity

building/space education (16th-18th Nov.) Group work on fabrication of an electric circuit system and discussion about

Cansat mission ISAS/JAXA tour (17th Nov.) Test launch of model rocket (19th Nov.)

Second week Mission and system definition review (21st Nov.) Akihabara tour (21st Nov.) Fabrication and testing of BBM of Cansat Lecture on nanosatellite engineering (22th Nov.) CDR (26th Nov.)

Third week Fabrication and testing of FM of Cansat

Fourth week Launch of Cansat by balloon and model rocket (6th Dec.) Post launch meeting (7th Dec.) Wrokshop on mbed microcomputer system (8th Dec.) Planning of education program in each country (8th-9th, Dec.)

Schedule of CLTP2


Homework kit Electric board

Schedule of CLTP2

Period Contents




Opening ceremony Briefing Lecture Group work JAXA tour Test launch

Schedule of CLTP2

Period Contents

Second week Mission and system definition review (M/SDR) (21st Nov.) Akihabara tour (21st Nov.) Fabrication and testing of BBM of Cansat Lecture on nanosatellite engineering (22th Nov.) Midterm report (CDR) (26th Nov.)

M/SDR

Akihabara tour BBM

Lecture

Midterm report

Schedule of CLTP2

Period Contents


testing

integration

drilling

DC-DC converter

parts and tools

CLTP laboratory

machining tools

parachute

PCB prototyping

Cansat

Cansat

Cansat carrier for balloon

Schedule of CLTP2

Period Contents


Cansat

Cansat

Drop test from balloon

Rocket launch

Post launch meeting

mbed workshop

Schedule of CLTP2





Second week Mission and system definition review (21st Nov.) Akihabara tour (21st Nov.) Fabrication and testing of BBM of Cansat Lecture on nanosatellite engineering (22th Nov.) CDR (26th Nov.)



The participants perfectly finished such a tight schedule!

CLTP2 Report

乾杯（かんばい)(KanPai)

KISSCANSATO

CLTP2 CANSAT MissionsRemote Sensing

Taking Photo and VideoAcquiring Atmospheric, Accelerometer and Position Data

TemperaturePressureGPS

Satellite housekeeping dataBattery VoltageSub‐system Life CheckEEPROM storageSub‐system Life Check

CommunicationSend data via XbeeGround station

OthersWithin Mass, volume, time and Yen Budgets

OBC:PIC16f877EEPROMADC

Pressure

+TEMPCAMERA+ SD

GPS

XbeeXCVR

BATTERY+

3.3v‐5V converter+ main pwr

sw

Sep. SW

PCParachute+

Harness+

structure

Team D

BalloonVideo

18.00

18.50

19.00

19.50

20.00

20.50

21.00

21.50

22.00

22.50

23.00

23.50

24.00

24.50

25.00

25.50

26.00

0.0 5.010.015.020.025.030.035.040.045.050.055.060.0

Tempe

rature

Time (seconds)

Balloon:Temperature Measurement

Balloon:Pressure Measurement

1012.001012.501013.001013.501014.001014.501015.001015.501016.001016.501017.001017.501018.001018.501019.001019.501020.001020.501021.001021.501022.001022.501023.001023.501024.001024.501025.001025.501026.001026.501027.00

0.0

3.5

7.0

10.5

14.0

17.5

21.0

24.5

28.0

31.5

35.0

38.5

42.0

45.5

49.0

52.5

56.0

59.5

Pressure (P

a)

Time (seconds)

‐4.50‐4.00‐3.50‐3.00‐2.50‐2.00‐1.50‐1.00‐0.500.000.501.001.502.002.503.003.504.004.50

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Time (seconds)

acc‐Y

acc‐X

Balloon Launch:X, Y and Z Acceleration Data

‐2.50‐2.00‐1.50‐1.00‐0.500.000.501.001.502.002.50

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Time (seconds)

Balloon Experiment, GPS Data

Rocket LaunchVideo

Rocket launch data - Dec 06, 2011

17

19

21

23

25

27

29

0 24 48 112

135

199

223

247

311

335

358

422

446

510

534

558

621

645

709

733

757

821

845

908

932

956

1020

1044

1108

1131

1155

1219

1243

1307

1331

1355

1418

1442

1506

1530

1554

1618

1641

1705

1729

1753

1817

1841

1905

1928

1952

Temperature

99000

99500

100000

100500

101000

101500

102000

102500

1030000 24 48 112

135

199

223

247

311

335

358

422

446

510

534

558

621

645

709

733

757

821

845

908

932

956

1020

1044

1108

1131

1155

1219

1243

1307

1331

1355

1418

1442

1506

1530

1554

1618

1641

1705

1729

1753

1817

1841

1905

1928

1952

Pressure


990.00991.00992.00993.00994.00995.00996.00997.00998.00999.001000.001001.001002.001003.001004.001005.001006.001007.001008.001009.001010.001011.001012.001013.001014.001015.001016.001017.001018.001019.001020.00

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Pressure (P

a)

Time (seconds)

15.0015.2515.5015.7516.0016.2516.5016.7517.0017.2517.5017.7518.0018.2518.5018.7519.0019.2519.5019.7520.0020.2520.5020.7521.0021.2521.5021.7522.00

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Tempe

rature

Time (seconds)

Rocket Launch:X, Y and Z Acceleration Data

‐4.50‐4.00‐3.50‐3.00‐2.50‐2.00‐1.50‐1.00‐0.500.000.501.001.502.002.503.003.504.00

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Time (seconds)

acc‐Y

acc‐X

‐2.50‐2.00‐1.50‐1.00‐0.500.000.501.001.502.002.50

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Time (seconds)


99000

99500

100000

100500

101000

101500

102000

102500

1030000 24 48 112

135

199

223

247

311

335

358

422

446

510

534

558

621

645

709

733

757

821

845

908

932

956

1020

1044

1108

1131

1155

1219

1243

1307

1331

1355

1418

1442

1506

1530

1554

1618

1641

1705

1729

1753

1817

1841

1905

1928

1952

Pressure

17

19

21

23

25

27

29

0 24 48 112

135

199

223

247

311

335

358

422

446

510

534

558

621

645

709

733

757

821

845

908

932

956

1020

1044

1108

1131

1155

1219

1243

1307

1331

1355

1418

1442

1506

1530

1554

1618

1641

1705

1729

1753

1817

1841

1905

1928

1952

Temperature

Rocket: Pressure Measurement

990.00991.00992.00993.00994.00995.00996.00997.00998.00999.001000.001001.001002.001003.001004.001005.001006.001007.001008.001009.001010.001011.001012.001013.001014.001015.001016.001017.001018.001019.001020.00

0.0

1.5

3.0

4.5

6.0

7.5

9.0

10.5

12.0

13.5

15.0

16.5

18.0

19.5

21.0

22.5

24.0

25.5

27.0

28.5

30.0

31.5

33.0

34.5

36.0

37.5

39.0

40.5

42.0

43.5

45.0

46.5

48.0

49.5

51.0

52.5

54.0

55.5

57.0

58.5

60.0

61.5

Pressure (P

a)

Time (seconds)

Rocket launch acceleration and Pressure data - Dec 06, 2011

Rocket Experiment, GPS Data

Over‐night Flight

Best photos

Rocket launch recovery photos

Comments on CLTP2 and CANSAT project

What is interesting is I get a lesson on the satellite‐making process from the expert and directly involved in the process using the CANSAT media from the beginning to the Balloon and Rocket Experiments with helping from Nihon Univ. students and also JAXA tour! – Agfianto Eko

Putra (Indonesia)I am very glad I had the chance to meet people who have

real experience in designing and getting satellites to orbits. In addition I gained experience in Japan ways of

exposing students with satellite technologies and development.‐ Syahrim Azhan Ibrahim (Malaysia)

Malaysia: Plan for the future

National Space Agency of Malaysia had organized CanSat competition for universities on

2007 & 2008.We plan to revive the workshop & competition

in 2012.Criteria:

‐Minimum success mission set by the organizer.‐Full success mission to be defined by

participants for us to see current progress.

Nigeria future plans of CANSAT activities

Our future plans is capacity building towards space related activities to our students, starting

from the basics of space systems (CANSAT development), hand on experiment/training , firstly to our universities, where we have our

space clubs then to other undergraduates within our nation.

Indonesia: Plan for the future

We have the Indonesian CanSat competition every year for all Universities in Indonesia, so its time to continue the tradition since 2008, KOMURINDOPlan to conduct CanSat Workshop for Universities

and High School Students, start 2012To be aligned with INSPIRE – Indonesia Nano Satellite

Project for Research and Education Consortium (established since 2010).

Establish the UGM Satellite Research and Development Center at the end of 2011 (now in

progress).

• Introduce CanSat to EE Undergrad through project work

• Outreach program for High School students

Future Plan at NTU‐Singapore

CANSAT Future Plan for Peru1. Continue activities with high school students through

CanSat Peru.2. Develop uC libraries and modules to enable high school

students, without any kind of electrical engineering background to successfully develop CanSats.

3. Find means to test CanSats through the use of water rockets, if possible.

4. Entail more seniors and bachelors in science to join the CanSat Peru project, so we can teach in more high schools.

5. As long term plans, to develop a CanSat competition for South America, and to increase the interest of Peruvian high school students in science and engineering, being this my primary motivation.

-Include CanSat in university’s curriculum for engineering-Organize space education and outreach, Yuri’s Night, World Space Week events-High altitude balloon, water and model rocket launching-February 2012: establishment of UNISEC Vietnam and CanSat program

-At least 3 universities initially: FPT University, Hanoi University of Science and Technology and Le Qui Don Technical University-Spread the words, start making CanSats in Vietnam

-August 2012: development and launching of CanSats developed by UNISEC Vietnam via high-altitude balloon or model rockets, first national CanSat contest-February 2013: double the number of universities to join UNISEC Vietnam (6)-September 2013: first Vietnamese CanSat team to join ARLISS contest in Japan or the US-February 2014: at least 10 universities in Vietnam have active CanSat / CubeSat program

Future plan for CanSat in Vietnam (milestones)

Future plan for CANSAT in Thailand

• We will conduct CANSAT training workshops for both high‐school and undergraduate university students.

• We will conduct a CANSAT competition on a Balloon launch.

• UNISEC Organization• Prof. Miyazaki• Nihon University Students

Thank you very much

CANSATO ‐ Final Report ‐ 07 Dec. 2011

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