Perkiraan Impuls Jenis (Isp) Propelan Komposit Padat. Berdasarkan Pengaruh Binder Sistem
| Main Author: | Heri Budi Wibowo |
|---|---|
| Format: | Book |
| Bahasa: | ind |
| Terbitan: |
LAPAN
, 2001
|
| Subjects: | |
| Online Access: |
http://repository.lapan.go.id//index.php?p=show_detail&id=6136 |
| ctrlnum |
slims-6136 |
|---|---|
| fullrecord |
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<dc schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd"><title>Perkiraan Impuls Jenis (Isp) Propelan Komposit Padat. Berdasarkan Pengaruh Binder Sistem</title><creator>Heri Budi Wibowo</creator><subject>Binder Sistem</subject><subject>Propelan</subject><publisher>LAPAN</publisher><date>2001</date><language>ind</language><type>Book:Book</type><identifier>http://repository.lapan.go.id//index.php?p=show_detail&id=6136</identifier><identifier>1412-2898</identifier><description>Abstrak Tulisan ini membahas suatu model untuk mementukan impuls jenis propelan komposit padat berdasarkan komposisi dan struktur bahan penyusun propelan. Bahan pengikat propelan dipilih dari bahan poliuretan dengan beberapa sistem PBAN, PBAA, Castor Oil dan Solithane C,00-300). Model perkiraan impuls :nis didatarkan pada panas reaksi pembakaran ideal dan berlaku keadaan adiabatis. Uji pembakaran propelan dilakukan pada tekanan bakar 30 atm dengan komposisi berat bahan pengikat : amonium perklorat : aluminium = 10 : 80 : 10. Propelan dibuat dengan metode casting. Hasil analysis data percobaan menunjukkan bahwa model perkiraan impuls jenis propelan cukup balk Bahcm pengikat sistem HTPB memberikan impuls jenis yang paling tinggi, diikuti berturut-turut PBAN, PBAA, Solithane C100_300, dan Castor Oil. Hasil simulasi terhadap komposisi TD1 yang digunakan juga diberikan. Abstract This paper described a model for determining Specifis impulse of solid composite propellant based on the composition and structure of raw materials. Polyurethane Binder selected was HTPB, PBAA, PBAN, Castor oil, Solithane C,00-300. The model to determine a specc impulse was based on the ideal heat of combustion at adiabatic state. Combustion test of propellant was conducted at combustion pressure 300 atm in Binder : Ammonium perchlorate : Aluminium = 10 : 80 : 10 pbw. The propellant was prepared by casting method. The analysis result on research data saw that the model to determine a specific impulse of propellant is adequate. The HTPB binder had the highest specific impulse, followed PBAN, PBAA, Solithane C100-300, and the lowest castor oil. The simulation result on TD1 composition is also given. </description><geographic>Bogor</geographic><description>Hlm. 9-14</description><subject>NONE</subject><recordID>slims-6136</recordID></dc>
|
| language |
ind |
| format |
Book:Book Book |
| author |
Heri Budi Wibowo |
| title |
Perkiraan Impuls Jenis (Isp) Propelan Komposit Padat. Berdasarkan Pengaruh Binder Sistem |
| publisher |
LAPAN |
| publishDate |
2001 |
| topic |
Binder Sistem Propelan NONE |
| url |
http://repository.lapan.go.id//index.php?p=show_detail&id=6136 |
| contents |
Abstrak Tulisan ini membahas suatu model untuk mementukan impuls jenis propelan komposit padat berdasarkan komposisi dan struktur bahan penyusun propelan. Bahan pengikat propelan dipilih dari bahan poliuretan dengan beberapa sistem PBAN, PBAA, Castor Oil dan Solithane C,00-300). Model perkiraan impuls :nis didatarkan pada panas reaksi pembakaran ideal dan berlaku keadaan adiabatis. Uji pembakaran propelan dilakukan pada tekanan bakar 30 atm dengan komposisi berat bahan pengikat : amonium perklorat : aluminium = 10 : 80 : 10. Propelan dibuat dengan metode casting. Hasil analysis data percobaan menunjukkan bahwa model perkiraan impuls jenis propelan cukup balk Bahcm pengikat sistem HTPB memberikan impuls jenis yang paling tinggi, diikuti berturut-turut PBAN, PBAA, Solithane C100_300, dan Castor Oil. Hasil simulasi terhadap komposisi TD1 yang digunakan juga diberikan. Abstract This paper described a model for determining Specifis impulse of solid composite propellant based on the composition and structure of raw materials. Polyurethane Binder selected was HTPB, PBAA, PBAN, Castor oil, Solithane C,00-300. The model to determine a specc impulse was based on the ideal heat of combustion at adiabatic state. Combustion test of propellant was conducted at combustion pressure 300 atm in Binder : Ammonium perchlorate : Aluminium = 10 : 80 : 10 pbw. The propellant was prepared by casting method. The analysis result on research data saw that the model to determine a specific impulse of propellant is adequate. The HTPB binder had the highest specific impulse, followed PBAN, PBAA, Solithane C100-300, and the lowest castor oil. The simulation result on TD1 composition is also given. Hlm. 9-14 |
| id |
IOS4589.slims-6136 |
| institution |
Lembaga Penerbangan dan Antariksa Nasional |
| institution_id |
623 |
| institution_type |
library:special library |
| library |
Repositori LAPAN |
| library_id |
1123 |
| collection |
Repositori Institusi LAPAN |
| repository_id |
4589 |
| subject_area |
The Universe/Alam Semesta, Jagat Raya, Alam Raya, Antariksa, Ruang Angkasa |
| city |
JAKARTA TIMUR |
| province |
DKI JAKARTA |
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1 |
| repoId |
IOS4589 |
| first_indexed |
2019-05-07T12:38:58Z |
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2019-05-07T12:38:58Z |
| recordtype |
dc |
| _version_ |
1686145346845016064 |
| score |
17.205004 |