The 3rd Regional Galaxy Forum Southeast Asia is taking place at the National Institute of Aeronautics and Space (LAPAN) branch office in Bandung, West Java, Indonesia. In addition to ILOA, the event is co-organized by the Institute of Technology Bandung (ITB). Faculty of the Department of Astronomy at ITB have been a key factor in the development of the regional SEA Galaxy Forum program. Indonesia, the world’s 4th most populous country, is building 21st Century capabilities and investing in the future of Astronomy and Astronautics to the immediate benefit of students in every class across the archipelago. Scientists at the Bosscha Observatory, ITB and others, continue with plans to construct a 2.5-m class telescope and a 1-m radio telescope at Mount Timau or Mount Rinjani. LAPAN is planning to complete work on a Space Port and Launch Center at Morotai Island by 2025. This complex is to act as the test site and future operational base of the LAPAN experimental satellite launcher. Last year the Rocket Technology Center conducted a successful static test of the RX 320 booster generating thrust of up to 4.9 tons. This is one of two rockets that will form the building blocks of the 4 stage orbital satellite rocket Roket Pengorbit Satelit (RPS) that is currently in development.

1. Indonesia Space Activities
Prof. Dr. Thomas Djamaluddin

2. Introduction
Space technology and information technology are the most important
technololgies in modern life, not only in global and national scale, but also
in personal activities.
Space technology is used for telecommunication, survaillance, and
navigation. Indonesia as maritime continent, with 13,466 named islands
(~17,000 islands, including no-name islands) needs space technology.
Since space technology is close
related to aeronautics
technology, Indonesia has
“National Institute of
Aeronautics and Space”, in
which space and aeronatics
(aerospace) science and
technology developments, as
well as policy studies, are
conducted.

3. A Brief History of Aerospace Activities
in Indonesia
• The Aviation Board was established on 1955 based on
Government Regulation No. 5/1955. This board later
changed to become the National Aeronautics and Space
Council of the Republic of Indonesia (DEPANRI) by
Presidential Decree No. 99/1993. DEPANRI is chaired by the
President of Republic of Indonesia with members consisting
of State Minitry of Research and Technology (also as vice
chairman and acting chairman), Minister of Foreign Affairs,
Minister of Trade and Industry, Minister of Defence, and
State Minister of Development Planning.
• Space technology activities in Indonesia started in the 1960s.
In 1962 PRIMA (Proyek Roket Ilmiah dan Militer Awal) – the
Primilinary Project on Scientific and Military Rocket was
stared. The first rocket produced by this project (i.e. Kartika)
was launched on 14 August 1964 from Launching Station at
Pameungpeuk, West Java.
• National Institute of Aeronautics and Space (LAPAN) was
established based on Presidential Decree No. 236/1963.
• In 1976 Indonesia became the third country using
telecommunication satellite, PALAPA.

4. • Space Law No.
21/2013 was enacted
on 6 August 2013.
A Brief History of Aerospace Policies
in Indonesia

5. Indonesian Space Policies
in Space Law No. 21/ 2013
• The space law consists of general policies related to space activities,
i.e. space science, remote sensing, aerospace technology mastery,
space launch and space commercial activities.
• LAPAN as government institution has authority to conduct of all
space activities in Indonesia, in addition to current duty as aerospace
research and development institution.
• LAPAN is directly responsible to the President of Indonesia, while its
activities are technically coordinated by a ministry for research and
technology.
• The space law is intended to promote self-sufficiency and national
competitiveness, to encourage space exploration and utilization for
national prosperity and productivity, to ensure space activity
sustainability, to provide law basis for space activities, to ensure
security and safety in space activities, to ensure the implementation
of international agreement, and to support national defence and
integrity.

6. STRUKTUR ORGANISASI

7. LAPAN MAIN COMPETENCES
SPACE SCIENCE &
ATMOSPHERIC
SCIENCE
AERONAUTICS &
SPACE TECHNOLOGY
REMOTE SENSING AERONAUTICS &
SPACE POLICY
Development of National
capability in utilizing of
remote sensing technology
for earth observation with
focus on development of
National Remote Sensing
Data Bank to support data
needs from Ministry, Local
Goverment, Military and
Police.
Development of
Unmanned Air Vehicle
(UAV/drone) & Air
Transport design, Satellite
Development & its
components and sounding
rocket development and its
spin off for peaceful
purposes
Development of Decision
Support System for space
Weather and dynamic of
equator atmosphere
Drafting of Government
Regulation and President
Regulation according to
National Decree on Space
and guidlines in
international forum.

8. LOCATION OF LAPAN FACILITIES
Jakarta
Rumpin
Bandung
Tanjungsari
Pameungpeuk
Watukosek
Rancabungur
Kototabang
Pontianak
Parepare
Biak

9. ROAD MAP OF SATELLITE TECHNOLOGY PROGRAM

10. LAPAN-A2 /
ORARI
LAPAN-A3 /
IPB
LAPAN-A1 /
TUBSAT
Mission Video Surveilence
Earth Surveilance, maritime monitoring,
Amateur Communication
Experimental remote sensing, maritime
monitoring, Science exp.
Payload
Analog Video Camera, Low
resolution VideoCam
Digital Space Camera, Analog Video Camera,
AIS, APRS
4 band pushbroom imager, Hi res DigitalCam,
AIS, APRS
Spectral resolution PAL Camera (752 x 582 pixel) Digital Camera (2048 x 2044 pixel)
Analog Camera (752 x 582 pixel)
450 - 520 nm; 520 - 600 nm;
630 690 nm; 760 - 900 nm
Spatial resolution 5 m ( 3,5 km swath),
200m (80 km swath)
4 m (7 km swath),
5 m (3,5 km swath)
18 m (100 km swath) / 4 m (7 km)
Orbit 635 km, 97,6 deg 650 km, 8 deg, Near-Equatorial 650 km, 97,6 deg
Data TX, and
TT&C
S-Band : 2220 MHz,
UHF : 437,325 MHz
S-Band : 2220 MHz,
UHF : 437,425 MHz
X-Band : 8116 - 8284 MHz,
UHF : 437,325 MHz
Downlink rate 5 Mbps 5 Mbps 105 Mbps
Total weight 57 kg 74 kg 115 kg
Dimension 450 x 450 x 270 mm 500 x 470 x 360 mm 500 x 500 x 700 mm
Launch 2007 2nd quarter 2015 End of 2015

11. Mision
Experimental remote sensing
(Validation of Optical data pre-
processing algorithm)
Experimental remote sensing.
(Development of SAR Micro-Sat for Maritime
and agriculture monitoring)
Payload Visible and Near Infrared imager
experimental,
Shyntetic Aperture Radar Experimental
(deployable dimension 450 x 70 cm), AIS
Spectral/discrimina-
tion mode
NIR Bolometer camera, Selectable
with 10 nm interval.
L-band; HH, HV, VH, VV polarimetry
Spatial resoluition 5 m ( 3,5 km swath), 1 km 30 m (100 km)
Orbit 650 km, 97,6 deg 650 km, 97,6 deg
Payload TX, TTC X-band, S-band X-Band, S-band
Downlink rate 200 Mbps 200 Mbps
Dimension Max 60x60x80 cm³ Max 60x60x80 cm³
Weight 150 kg 200 kg
LAPAN-A4
LAPAN-A5

12. LAPAN’s Equatorial Satellite Mission
• Meanwhile, the temporal resolution of patrol-boat-based radar and AIS receiver is
very low considering the vast water region. Therefore, satellite-based AIS is truly a
solution for Indonesian problem combining with UAV and SAR satellite technology.
• Since Indonesian territory is spread along the equator, LAPAN decide the operation of
maritime surveillance satellite at the beginning at low inclination orbit, so that the
satellite may pass Indonesia as much as SSO orbit pass the North/South pole (14
times in 24 hours at 650 km orbit).

13. Space-borne AIS for Maritime Surveillance
• AIS (Automatic Identification System) is a system that can monitor ships, based
on GPS and VHF digital communication. It is regulated by IMO to be installed in
ships weighing 300 tons and above.
• By placing AIS receiver on the satellite, its coverage will
be larger compared to the one usually placed on
the seashore by maritime authority.

14. Technological Feasibility
The development of satellite-based AIS has been done since 2007
by the US military experimental satellite TACSAT-2. At the moment,
commercial entities like Orbcomm, Com Dev, SpaceQuest dan
Kongsberg Seatex has developed satellite AIS receiver.
Plot of AIS Messages Collected by Nano-satellite
Tracking of Ships (NTS) - Canada

15. Standard AIS can detect 1000 ships by 15 minutes observation (probability >90%)
Space-borne AIS : 2000 ships detection by 10 minutes observation (probability >90%)
Standard AIS
Technological Feasibility
Ship Detection Probability by AIS at 1000 km Altitude

16. LAPAN-A2 AIS System

17. Software Processing
G/S Software:
Acquisition Data from G/S Receiver
Process Raw:
• Remove Frame Counter
• Separating AIS Data from Idle Package
• Filtering AIS data with CRC
Formatting AIS Data:
• As Text File
• As Shipplotter Format
• As Ship NMEA Format
• As Google Earth KML Format
• Tracking Special Ship
AIS Data Ground Processing
LAPAN-A2 AIS System

18. LAPAN-A2 satellite will be launched as auxiliary payload on PSLV
mission at 2nd semester of 2015.
LAPAN-A2 AIS System

19. LAPAN-A3/IPB SATELLITE
(An Experimental Remote Sensing Satellite)
• Cooperate with Bogor Agricultural University (IPB) for payload
specification
• Orbit: ~650 km, 97,6 deg
• Payload;
 Experimental remote sensing, maritime monitoring, Science exp.
 4 band pushbroom imager (450 - 520 nm; 520 - 600 nm; 630 690 nm; 760 -
900 nm), Hi res DigitalCam, AIS, APRS
 ~18 m (~100 km swath) Multispectral/ ~4 m (~7 km) Matrix RGB
 115 kg
 End of 2015
• Weight: ~115 Kg

20. Satellite Development Capabilities
• In-house design capabilities
• In-house Satellite Assembly, Integration & Test (AIT) with thermal,
vacuum chamber, Uniform Light Source, 10,000 & 100,000 clean room
class.
• Customize Satellite operation software
• Satellite Platform and structure manufacturing
• TTC and image reception satellite operation
• In-house satellite components development: (Reaction wheels, Magnetic
coils, Star Tracker, On Board Data Handling)
• Image systematic pre-processing, (Geometric, Radiometric correction,
atmosferic refraction & dispersion, blurring distortion, stochastic
distorsion)

21. AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
LAPAN SURVEILLANCE UAV (LSU)

22. LSU Program Status
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

23. VARIAN PROTOTYPE LSU
LSU-01
 Wing tail : 1900 mm
 Lenght : 1200 mm
 Take off : launch
 Maximum Payload : 0,5 kg
 Speed : 45 km/jam
 Max speed : 60 km/jam
 Airspeed Stall : 30 km/jam
 Machine : Brushless
 Fuel : Battery
 Max flight time : 50 menit
 Control System :
Take off/landing by remote control &
fly by autonomous
LSU-02
 Wing tail : 2400 mm
 Lenght : 1700 mm
 Maximum Payload : 3 kg
 Speed : 100 km/jam
 Max speed : 150 km/jam
 Airspeed Stall : 40 km/jam
 Machine : 2 Tax 32cc
 Fuel :
Pertamax plus & oli full sintetic
 Tank : 3,5 liter
 Max flight time : 3,8 jam
 Control System :
Take off/landing by remote
control and fly by
autonomous
 LSU-03
 Wing tail : 3500 mm
 Lenght : 2500 mm
 Tail Height : 700 mm
 Center Wing : 900 mm
 Speed : 100 km/jam
 Max speed : 150 km/jam
 Airspeed Stall : 60 km/jam
 Maximum Payload : 10 kg
 Machine : 2 Tax 100cc
 Fuel :
Pertamax Plus & Oli Full Sintetic
 Tank : 7 liter
 Max flight time : 5 jam
 Control System :
Take off/landing by remote control and fly
by autonomous
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

24. VARIAN PROTOTYPE LSU
LSU-04
 Wing tail : 4000 mm
 Lenght : 3200 mm
 MTOW : 65 kg
 Speed : 100 km/jam
 Max speed : 160 km/jam
 Airspeed Stall : 60 km/jam
 Maximum Payload : 18 kg
 Machine : 11 HP
 Tank :
Pertamax plus &oli full sintetic
 Tank : 8 liter
 Max flight time : 6 jam
 Control System:
Take off/landing by remote control &
flight by autonomous
LSU-05
 Wing tail : 5500 mm
 Lenght : 4100 mm
 Height : 1130 mm
 MTOW : 77 kg
 Empty Weight : 31 kg
 Payload Mass : 30 kg
 Fuel : 16 kg
 Take Off Ground Round : 60 meter
 Climb Rate : 600 ft/min
 Range : 840 km
 Endurance : 8 h
 Lending Ground Run : 83 meter
 Ceiling : 12000 ft
 Cruise Altitude : 3000 ft
 Cruise speed : 100km/h
FADEX
 Wing tail : 3500 mm
 Lenght : 2800 mm
 Take Off mass : 10 kg
 Cruise Speed : 160 km/jam
 Cruise Altitude : 1000 m
 Max flight time : 0,5 jam
 Proppeller : Turboshaft
 Machine : 20 HP - 30 cc
 Fuel : gasoline
 Payload : 15 kg
 Tank : 2 liter
 Airframe : Composite
 Control System:
Take off/landing by remote control &
flight by autonomous
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

25. Program LSU progame achievement status
LSU 02 in military 2012-2013
( Ship On Board Take Off and Landing )
Battlefield maping, Dittop AD 1200 Ha (± 7 hours )
MURI record achievment (200 KM Autonumous)
Flood monitoring
REMOTE SENSING DATA
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

26. LAPAN SURVEILLANCE AIRCRAFT (LSA)
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

27. Status program LSA - AADP - UAV Research and Development of UAV :1 ton MTOW
- Light and advanced Aircraft Research and Development
( Autonomous Control & Composite )
- Simulator System
- Capacity Building (Master and Phd)
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

28. LSA’s Program status
Parameter Pengambilan Sample Lapangan
Kondisi periode tanaman padi
Biomas tanaman padi
Tinggi tanaman padi
Kerapatan tanaman
Variabel fisik lainnya
0
SPESIFIKASI PESAWAT CESSNA 206
- Mesin : C
o
ntinental IO-520-A 285 hp (213 kW)
- Tempat D
u
duk : one (crew) & five passengers
- Length : 8,61 m
- Wingspan : 10,97 m
- Height : 2,83 m
- Wing Area : 16,3 m2
- Airfoil : N
A
CA 2412
- Berat Ko song : 987 kg
- Max. Takeoff We i ght : 1.632 kg
Performance
Kecepatan Maksimum : 151 knots (280 km/h)
Kecepatan Cr uise : 142 knots (263 km/h)
Kecepatan Stall : 54 knots (100 km/h)
Jarak Tempuh : 840 mi (730 nmi, 1.352 km)
Serving ceiling : 15.700 ft (4.785 m)
A
Deskripsi LSA-S15
Pesawat terbang ringan
Untuk melakukan misi surveillance seperti pemetaan, monitor-­
ing, SAR dan lain se bagainya.
Pesawat ini mempunyai basic design berupa pesawat glider bermo-­
tor,
Airframe pesawat terbuat dari komposit dengan rangka utama terbuat
dari batang logam s
i
li nder.
Memiliki desain modular airframe yang dapat memudahkan pesawat
diangkut dengan bagian ya ng terpisah-pisah.
SPESIFIKASI PESAWAT STEMME S – 15
-Tipe : Sayap Tetap, Retractable Landing Gear
- Airframe : C
a
rbon Fiber & Glass Fiber C
o
mposites
- Mesin : Tunggal – ROTAX 914 F2 (4 cylinder 4 stroke)
- Tempat D
u
duk : D
u
al (side by side)
-
Bahan Ba kar : AVGAS UL 91 atau 110LL
- Jarak Tempuh : sampai dengan 604 nm/1119 km (75% power, 97 knot
- Durasi Terbang : sampai dengan 6 jam 13 menit (FF 20.4 ltr/jam)
- Service C
e
iling : Max 16.000 feet
- Panjang Landasan yang dibutuhkan
Take Off : Ground R
o
ll 425 m, 50ft obstacle 833m
Landing R
o
ll : (tidak disebut dlm POH, lebih pendek drpd T/O)
Gradient T/O : 591 ft/mnt – 3m/sec
- Maks B
e
rat :1100 kgs
- Payload : sampai dengan 148 kgs (1 pilot 70kg)
- Minimal Crew : 1 (satu) orang
POD Kamera
Kamera & Rangkaian Kamera
Pemanfaatan :
MAINTENANCE
Parameter Pengambilan Sample Lapangan
Kondisi periode tanaman padi
Biomas tanaman padi
Tinggi tanaman padi
Kerapatan tanaman
Variabel fisik lainnya
0
- Length : 8,61 m
- Wingspan : 10,97 m
- Height : 2,83 m
- Wing Area : 16,3 m2
- Airfoil : N
A
CA 2412
- Berat Ko song : 987 kg
- Max. Takeoff We i ght : 1.632 kg
Performance
Kecepatan Maksimum : 151 knots (280 km/h)
Kecepatan Cr uise : 142 knots (263 km/h)
Kecepatan Stall : 54 knots (100 km/h)
Jarak Tempuh : 840 mi (730 nmi, 1.352 km)
Serving ceiling : 15.700 ft (4.785 m)
A
Deskripsi LSA-S15
Pesawat terbang ringan
Untuk melakukan misi surveillance seperti pemetaan, monitor-­
ing, SAR dan lain se bagainya.
Pesawat ini mempunyai basic design berupa pesawat glider bermo-­
tor,
Airframe pesawat terbuat dari komposit dengan rangka utama terbuat
dari batang logam s
i
li nder.
Memiliki desain modular airframe yang dapat memudahkan pesawat
diangkut dengan bagian ya ng terpisah-pisah.
- Mesin : Tunggal – ROTAX 914 F2 (4 cylinder 4 stroke)
- Tempat D
u
duk : D
u
al (side by side)
-
Bahan Ba kar : AVGAS UL 91 atau 110LL
- Jarak Tempuh : sampai dengan 604 nm/1119 km (75% power, 97 knot
- Durasi Terbang : sampai dengan 6 jam 13 menit (FF 20.4 ltr/jam)
- Service C
e
iling : Max 16.000 feet
- Panjang Landasan yang dibutuhkan
Take Off : Ground R
o
ll 425 m, 50ft obstacle 833m
Landing R
o
ll : (tidak disebut dlm POH, lebih pendek drpd T/O)
Gradient T/O : 591 ft/mnt – 3m/sec
- Maks B
e
rat :1100 kgs
- Payload : sampai dengan 148 kgs (1 pilot 70kg)
- Minimal Crew : 1 (satu) orang
POD Kamera
Kamera & Rangkaian Kamera
Pemanfaatan :
MODIFICATION POD
APPLICATION
Stu dy Ar ea
Subang – Indramayu, Jawa Barat
• Lahan sawah : irigasi dan tadah hujan
11
Subang
Jalur terbang LSA
Titik pengamatan
Indramayu
Descending
Ascending
Akuisisi Radarsat
APPLICATION TEST
BBSDLP-PUSTEKDATA-PUSTEKBANG
Cessna 2
0
6 PK-LPNLSA (LAPAN SU RVEILLANCE AIRCRAFT)
SPESIFIKASI PESAWAT CESSNA 206
- Mesin : C
o
ntinental IO-520-A 285 hp (213 kW)
- Tempat D
u
duk : one (crew) & five passengers
- Length : 8,61 m
- Wingspan : 10,97 m
- Height : 2,83 m
- Wing Area : 16,3 m2
- Airfoil : N
A
CA 2412
- Berat Ko song : 987 kg
- Max. Takeoff We i ght : 1.632 kg
Performance
Kecepatan Maksimum : 151 knots (280 km/h)
Kecepatan Cr uise : 142 knots (263 km/h)
Kecepatan Stall : 54 knots (100 km/h)
Jarak Tempuh : 840 mi (730 nmi, 1.352 km)
Serving ceiling : 15.700 ft (4.785 m)
PUSTEKBANG L
A
PAN RU MPIN
Jl. R
a
ya L
A
PAN, S
u
k amulya Ru mpin—Bogor
Deskripsi LSA-S15
Pesawat terbang ringan
Untuk melakukan misi surveillance seperti pemetaan, monitor-­
ing, SAR dan lain se bagainya.
Pesawat ini mempunyai basic design berupa pesawat glider bermo-­
tor,
Airframe pesawat terbuat dari komposit dengan rangka utama terbuat
dari batang logam s
i
li nder.
SPESIFIKASI PESAWAT STEMME S – 15
-Tipe : Sayap Tetap, Retractable Landing Gear
- Airframe : C
a
rbon Fiber & Glass Fiber C
o
mposites
- Mesin : Tunggal – ROTAX 914 F2 (4 cylinder 4 stroke)
- Tempat D
u
duk : D
u
al (side by side)
-
Bahan Ba kar : AVGAS UL 91 atau 110LL
- Jarak Tempuh : sampai dengan 604 nm/1119 km (75% power, 97 knot
- Durasi Terbang : sampai dengan 6 jam 13 menit (FF 20.4 ltr/jam)
- Service C
e
iling : Max 16.000 feet
- Panjang Landasan yang dibutuhkan
Take Off : Ground R
o
ll 425 m, 50ft obstacle 833m
Landing R
o
ll : (tidak disebut dlm POH, lebih pendek drpd T/O)
Gradient T/O : 591 ft/mnt – 3m/sec
- Maks B
e
rat :1100 kgs
- Payload : sampai dengan 148 kgs (1 pilot 70kg)
- Minimal Crew : 1 (satu) orang
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

29. NATIONAL TRANSPORTATION
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

30. Program Status of N-219
TRANSFER OF TECHNOLOGY
14 SPESIALIS
WIND TUNNEL TEST
PROCUREMENT (60-70%) &
DETAIL DESIGN(90%)
FIRST CUTTING DETAIL
PART MANUFACTURING
ROLL OUT 10 AGUSTUS 2015
FIRST FLIGHT DESEMBER 2015
AERONAUTICS TECHNOLOGY DEVELOPMENT PROGRAM
(cont’d)

31. LAPAN has been succesfully launched its rockets in Pameungpeuk Test Flight Station, Jawa Barat since 2008, RX-
320 on 2008, 19 May and RX-420 on 2009, 2 July. Moreover LAPAN were already testing on RX-550 mainly static
test in 2011 and 2012. Further work LAPAN is going to retest RX 420. Meanwhile for RX-550, the bigest rocket
developed by LAPAN wish make its flight test in 2015.
• 2008 : RX-320 STATIC &
FLIGHT TEST
• 2009 : RX-420 STATIC &
FLIGHT TEST
• 2010 : RX-550 DESIGN
• 2011 : RX-550 STATIC TEST
• 2012 : RX-550 STATIC TEST
• 2013 : RX-550 (SINGLE
STAGE) FLIGHT TEST
• 2014 : RX-550 (DOUBLE
STAGES) FLIGHT TEST
Currently status :
LAPAN’s satellite
launcher called
Rocket Sonda
designing and
integrating
autonomously.
ROAD MAP OF ROCKET TECHNOLOGY PROGRAM

32. Succesfully flown
RSX 100 / RX 1210
RX 320 Succesfully flown
Static test RX 450
Static test
RCX 100H2 (liquid rocket)
Space port In
Morotai Island
PROGRAM STATUS OF ROCKET TECHNOLOGY
Succesfully flown
RKX EDF / RKX TJ

33. Informasi lahan sawah
Kabupaten OKU Timur
Several activities such as distribution of mid and
high resolution data to user have been already
done by Lapan to implementing the Inpres No. 6,
2012, about “Provision, Utilyzing, Quality
Control, Proccesing and Distributing High
Resolution Remote Sensing Data”. In oder to
strengthen those activities, Lapan also has
received and distributed LDCM/ Landsat-8’s
data to user; ie. K/L, local government,
TNI/Police, and private Mei 3, 2013,

34. Strenghtening Facility
Antena X-band
6.1 meter
Antena X-band
5,4 meter
Antena X-band
6.1 meter (Rumpin)
Antena L-band
1,5 meter (Pekayon)

35. Data Aquisition Area

36. Receiving, Processing and Management Remote
Sensing Data System
SPOT-5 /6 data receiving and
processing systems
Controlling room
Antenna control
system
Receiving and Processing Data System In
Balai Penginderaan Jauh Parepare
Processing and management data
system in Jakarta
MODIS and NPP
data processing
systems
Landsat data
processing
system
Database Server

37. Data Availability until 2014ata)
Spatial Res Data Period Locations
Low MTSAT-1R Okt 2008 – Now Indonesia
Feng Yun-1D 2003 – 2011 Indonesia
NOAA-18 2005 – Now Indonesia
NOAA-19 2009 – sekarang Indonesia
Terra/Aqua 2006 – sekarang Indonesia
NPP Feb 2012 – sekarang Indonesia
Mid ALOS AVNIR 2006 – 2011 Jawa, Sumatera, Bali, Nusa
Tenggara, Kalimantan
SPOT-2 Apr 2006 – Jun 2009 Indonesia
SPOT-4 Apr 2006 – Jan 2013 Indonesia
Landsat-5 1990 – 2009 Indonesia
Landsat-7 2001 – sekarang Indonesia
Landsat-8 Apr 2013 – sekarang Indonesia
Rapid Eye 2012 -2013 Kalimantan, Jawa, Sumatera

38. Data Availability (cont’d)
Spatial Res Data Period Locations
High SPOT-5 2005, Jan 2013 – now Sumatera, Jawa, Sulawesi, Nusa
Tenggara, Kalimantan, Papua
SPOT-6 Jan 2013 – now Sumatera, Jawa, Papua, Sulawesi,
Kalimantan
Pleiades Jun 2013 – now Province and cities in Indonesia
ALOS Prism Jun 2006 – Oct 2009 Jawa, Sumatera, Bali, Nusa Tenggara,
Kalimantan, Papua
Ikonos 2000 – 2004, 2007,
2008, 2011
NAD, Papua, Jakarta, Jateng, Jatim,
Papua
Quickbird 2006 – 2010 Sumatera, Kalimantan, Papua, Jabar,
Jatim
World View 2010 – 2012 Maluku, Papua
Geo Eye 2009 – 2011 Maluku, Papua, Jawa
SAR TerraSAR-X 2010 – 2013 Jakarta, Riau, Jambi, Kalteng, Kaltim,
Jateng, L. Timor, Nusa Tenggara
ALOS Palsar 2006 – 2010 Kalimantan, Sumatera, Jawa
Radarsat 2009 – 2010 Kalimantan

39. SPOT-7SPOT-6
Landsat-9Landsat-8 (LDCM)
Himawari-8Himawari-7
JPSS-1
MetOp-C
NPP
2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022
Terra
Aqua
NOAA-19
Himawari-6
SPOT-4
Landsat-7
SPOT-5
ALOS-2
SAOCOM-1A
FY-3FFY-3EFY-3DFY-3CFY-3B
Daily acquired
Planed in 2012
Planed below 2013
Acquisition Planing (2012-2020)

40. PROGRAM ACHIEVEMENT AND
REMOTE SENSING ACTIVITY
1. Indonesia’s National Carbon Accounting System (INCAS)
2. Development of Remote sensing data bank, Bank Data Penginderaan Jauh Nasional (BDPJN)  UKP4
and BIG
3. Supporting;
a. Maritim
- ZPPI, coral reef, mangrove and mariculture
b. Mitigation
SPBK, hotspot, potentatial flooding, disater emergency respons, active vulcanos information.
c. Natural Resources and environtment
Paddy growth phase, rural areas, cloud
4. Academic advisor  mahasiswa ITS, IPB, UGM, UI, UNNES, UB, etc),
Directing  Ditjenbun, BBSDLP, BPBD Kalbar, Dishut Riau, Ditjen PHKA, Kanwil Pajak Jateng, etc
Servicing  KLH, BBSDLP, Dinas Perikanan, BPPT, Ditjen PHKA, UKP4, etc)
Informasi Spasial Zona Potensi
Penangkapan Ikan (ZPPI)
Environment development and disaster
mitigation
Development model for Disaster mitigation of
vulcano maping
Forest land and
Kalimantan island forest
(2000-2009)
Forest land and Sumatera
island forest (2000-2009)

41. 41
5. Contributing in Reducing Emissions from Deforestation and
Forest Degradation (REDD+ Nasional), where LAPAN
succesfully developed near real time information system for
forest monitoring in order to fulfill UKP4 need; ie.. Daily
Normalized Difference Vegetation Index (NDVI) daily and
daily NDVI 16-daily including composite image. Terra/Aqua
MODIS in 2009-2012 based on Google Earth.
6. International organizations, such as LandGate Australia,
JAXA, ASEAN Secretariat, UN WFP, UN SPIDER, UN ESCAP,
CARE International, GIC-AIT, ADRC, and WWF also use
Remote sensing information to support disaster mitigation,
and Sentinel data completed the aerial data and Carbon
Accounting System.
PROGRAM ACHIEVEMENT AND
REMOTE SENSING ACTIVITY
(cont’d)

42. SPACE AND ATMOSPHERE SCIENCE
Space Weather Monitoring
Space Debris
Communication Frequency Area
Prediction
Development of early warning
systems and disaster mitigation
base on satellite act an early
warning system of rain fall
(Sahadev version 2.0). Sadewa
(Satellite Disaster Early Warning
System) or Disaster early
warning system base on MTSAT
Space debris monitoring cooperate with BAPETEN
for measuring the impact of space object radiation
Dissemination of ionosphere information utilization
for radio communications and Single Frequency of GPS
measurement, have been widely used, especially by
the military.
R&D result of space weather
monitoring is sosialized to
related institutions such as
:BMKG, PPGL, Basranas,
Bappeten, Angkasa Pura, TNI
AU, LPD Sumedang,BPD
Pontianak, BPD
Watukosek, BPPR
Pameungpek, Dislitbang TNI –
AU,Mahasiswa Politeknik Pos
Indonesia, Universitas Telkom

43. SPACE WEATHER MONITORING NETWORK

44. -Radio communication
frequency monitoring inter
locations (real time)
-Ionosonda data real time
Radio communication
frequency prediction
(monthly)
Sintilasi appearance
prediction(monthly)

45. ASTINA :
Is a multi-media display of an information
system in the field of atmospheric science
and technology which are constructed as a
component of a decision support system to
help users obtain information in accordance
with the requirements as the basis for
decision-making and policy-related sectors
such as information services: weather,
climate, agriculture, transportation, energy,
environment, water resources, health,
disaster management and education.
ASTINA ROOM

46. • Parameter information of
Indonesia’s atmosphere
based on Google Earth :
MTSAT ir-1, Ch-TRRM,
Ch prediction,
resolution 5 km and 50 km
1. ARJUNA : AtmospheRic JoUrNey Arcade
(Lorong Penjelajahan Atmosfer)
Arjuna is a three-dimensional visual media where users can conduct exploration
into the Earth's atmosphere to see the satellite-based observations, radar,
airborne and in situ, as well as the prediction of atmospheric conditions short,
medium and long-based dynamic models and statistical
ASTINA ROOM COMPONENTS :

47. National Space Development Master Plan
• In the Space Laws No. 21/2013, it is mentioned that LAPAN should
prepare a Master Plan for the implementation of national space
guidelines. The master plan drawn up for a period of 25 (twenty five)
years. Therefore, the current master plan is being drawn up, both
academic and legal draft of President Regulation. The master plan
has been proposed as one of national legislation program (prolegnas)
in 2014.
• The master plan will be prepared taking into account basic
capabilities and the national and international strategic environment.
The master plan contains the vision and mission, policies, strategies
and short, medium, and long-term strategic plans.

48. • The main issues in the master plan includes
• the construction of national observatory to support space science;
• to strengthen national remote sensing data bank;
• to strengthen aeronautics technology for developing UAV (Unmanned
Aerial Vehicle) and transport aircraft;
• to develop national satellite for remote sensing, telecommunication, and
navigation, starting from developing micro-satellite;
• to develop rockets for satellite launching, starting from developing
sounding rockets;
• and to build aerospace port in Eastern Indonesia;
• as well as to strengthen space policy studies.
• To enhance public awareness, space science and technology education
center should be built in locations of LAPAN’s station all over Indonesia.
• The national aerospace master plan should be supported by preparing
human resources and related industries.
• National and international cooperation on space science, technology, and
policy studies should be encouraged.
National Space Development Master Plan

49. THANK YOU