Synopsis
The project upgrades the GSLV Mk‑III solid booster via a high‑density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m³. An 8‑lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressive→neutral burn over ~110-120 s; the grain is carbon‑fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit Ø 2.36 m), and a carbon‑carbon throat coated with ZrC is optimized for sea‑level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity ≈2,714 m/s, Isp ≈277 s, mass flow ≈2,138 kg/s.
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
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LAP LAMBERT Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
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ISBN 10: 6209083625
ISBN 13: 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
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LAP LAMBERT Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
New
Paperback
Seller: Grand Eagle Retail, Bensenville, IL, U.S.A.
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. The project upgrades the GSLV Mk-III solid booster via a high-density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m3. An 8-lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressiveneutral burn over 110-120 s; the grain is carbon-fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit O 2.36 m), and a carbon-carbon throat coated with ZrC is optimized for sea-level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity 2,714 m/s, Isp 277 s, mass flow 2,138 kg/s. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Seller Inventory # 9786209083624
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OPTIMIZATION OF GRAIN AND NOZZLE GEOMETRY IN SOLID ROCKET BOOSTER GSLV
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The project upgrades the GSLV Mk III solid booster via a high density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m . An 8 lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressive neutral burn over ~110-120 s; the grain is carbon fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit Ø 2.36 m), and a carbon carbon throat coated with ZrC is optimized for sea level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity =2,714 m/s, Isp =277 s, mass flow =2,138 kg/s. 60 pp. Englisch. Seller Inventory # 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
New
Paperback
Seller: AussieBookSeller, Truganina, VIC, Australia
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. The project upgrades the GSLV Mk-III solid booster via a high-density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m3. An 8-lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressiveneutral burn over 110-120 s; the grain is carbon-fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit O 2.36 m), and a carbon-carbon throat coated with ZrC is optimized for sea-level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity 2,714 m/s, Isp 277 s, mass flow 2,138 kg/s. This item is printed on demand. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability. Seller Inventory # 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
New
Softcover
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv (Paperback)
Published by
LAP Lambert Academic Publishing, 2025
ISBN 10: 6209083625
ISBN 13: 9786209083624
New
Paperback
Seller: CitiRetail, Stevenage, United Kingdom
Seller rating 5 out of 5 stars
Paperback. Condition: new. Paperback. The project upgrades the GSLV Mk-III solid booster via a high-density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m3. An 8-lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressiveneutral burn over 110-120 s; the grain is carbon-fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit O 2.36 m), and a carbon-carbon throat coated with ZrC is optimized for sea-level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity 2,714 m/s, Isp 277 s, mass flow 2,138 kg/s. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Seller Inventory # 9786209083624
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