固化降温过程中无喷管助推器药柱结构完整性分析.
- Published in:
- Aero Weaponry, 2025, v. 32, n. 2, p. 121, doi. 10.12132/ISSN.1673-5048.2024.0132
- By:
- Publication type:
- Article
Works matching DE "ROCKET engines"
Results: 768
1
2
Operation of a Cryogenic Rocket Engine: an Outline with Down-to-Earth and Up- to-Space Remarks.
- Published in:
- 2011
- By:
- Publication type:
- Book Review
3
Consideration of fuel and oxidizer combinations for mass and volume limited hybrid rocket motors.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 9, p. 1, doi. 10.1002/prep.202400149
- By:
- Publication type:
- Article
4
Research progress and prospects on agglomeration models and simulation methods of aluminum particles in aluminum‐based composite propellants.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 8, p. 1, doi. 10.1002/prep.202400056
- By:
- Publication type:
- Article
5
A model for the combustion behavior of AP/HTPB propellant containing ultrafine aluminum.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 7, p. 1, doi. 10.1002/prep.202400049
- By:
- Publication type:
- Article
6
Thermal structural damage and thermal decomposition characterization of GAP propellants with nitrate ester plasticizers.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 5, p. 1, doi. 10.1002/prep.202300331
- By:
- Publication type:
- Article
7
Numerical simulation of the effect of multiple factors on the ignition process of a solid rocket motor.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 5, p. 1, doi. 10.1002/prep.202300198
- By:
- Publication type:
- Article
8
A constitutive model of solid propellants considering aging and confinement pressure.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 4, p. 1, doi. 10.1002/prep.202300286
- By:
- Publication type:
- Article
9
Light transmittance measurement method of solid rocket motor plume based on laser modulation spectrum analysis.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 3, p. 1, doi. 10.1002/prep.202300224
- By:
- Publication type:
- Article
10
Shear creep analysis of solid rocket motor bonding interface and rapid prediction model.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 3, p. 1, doi. 10.1002/prep.202300070
- By:
- Publication type:
- Article
11
Exploring the potential of boron carbide in enhancing energy output of solid fuels for SFRJ and hybrid rocket propulsion systems.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 1, p. 1, doi. 10.1002/prep.202300173
- By:
- Publication type:
- Article
12
Effects of micro and nano fillers on the mechanical and thermal properties of hydroxyl‐terminated polybutadiene‐polyurethane based rocket motor liner.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2024, v. 49, n. 1, p. 1, doi. 10.1002/prep.202300119
- By:
- Publication type:
- Article
13
Study on the constitutive model of NEPE propellant based on indentation creep.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 12, p. 1, doi. 10.1002/prep.202300169
- By:
- Publication type:
- Article
14
Rapid optimization method of solid rocket motor propellant with structural strength.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 11, p. 1, doi. 10.1002/prep.202300045
- By:
- Publication type:
- Article
15
Study on mechanical properties of solid propellant NEPE.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 8, p. 1, doi. 10.1002/prep.202200338
- By:
- Publication type:
- Article
16
Development of Mid‐Way Testing Contingencies for Solid Rocket Motor Processing.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 3, p. 1, doi. 10.1002/prep.202200316
- By:
- Publication type:
- Article
17
Identification of Viscoelastic Parameters for Composite Propellant by Indentation Technique.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 3, p. 1, doi. 10.1002/prep.202200309
- By:
- Publication type:
- Article
18
Theoretical Conditions for Burning in Solid Propellant Slots.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2023, v. 48, n. 3, p. 1, doi. 10.1002/prep.202200281
- By:
- Publication type:
- Article
19
Investigating the Acoustic Response Characteristics of a Solid Rocket Motor Combustor in High‐Temperature and High‐Pressure Environments.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 12, p. 1, doi. 10.1002/prep.202200108
- By:
- Publication type:
- Article
20
Micromechanical Behavior of HTPB Propellant Bonding Interface under Uniaxial Tensile Loading.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 10, p. 1, doi. 10.1002/prep.202200106
- By:
- Publication type:
- Article
21
A Nonlinear Ultrasonic Method for Detection and Characterization of Dewetting Damage in Solid Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 10, p. 1, doi. 10.1002/prep.202200079
- By:
- Publication type:
- Article
22
Using Wavy Fuel Surface to Improve the Performance of the Solid Fuel Ramjets.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 10, p. 1, doi. 10.1002/prep.202200061
- By:
- Publication type:
- Article
23
Are All Solid Propellant Burning Rate Modifiers Catalysts?
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 9, p. 1, doi. 10.1002/prep.202200148
- Publication type:
- Article
24
Long‐Term and Short‐Term Creep Characteristic Analysis for HTPB Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 9, p. 1, doi. 10.1002/prep.202200074
- By:
- Publication type:
- Article
25
On the Use of Fluorine‐Containing Nano‐Aluminum Composite Particles to Tailor Composite Solid Rocket Propellants.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 7, p. 1, doi. 10.1002/prep.202100370
- By:
- Publication type:
- Article
26
Assessment of Mechanical Properties of Aged Composite Propellant Using Non‐Destructive Indentation Technique in Solid Propellant Rocket Motor.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 6, p. 1, doi. 10.1002/prep.202100339
- By:
- Publication type:
- Article
27
Effects of Dense Inert Particle Loading in Shocked Energetic Materials.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 6, p. 1, doi. 10.1002/prep.202100330
- By:
- Publication type:
- Article
28
Effect of Protrusion on Combustion Stability of Hybrid Rocket Motor.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 4, p. 1, doi. 10.1002/prep.202100067
- By:
- Publication type:
- Article
29
Using Surface Grooves on Propellant Grain to Control the Erosive Burning in Solid Rocket Motors.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 2, p. 1, doi. 10.1002/prep.202100242
- By:
- Publication type:
- Article
30
Dissection Method of Solid Rocket Motor Chamber Based on Ultrasonic Vibration Sawing.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 2, p. 1, doi. 10.1002/prep.202100153
- By:
- Publication type:
- Article
31
The Curing Reaction Rate of the Rocket Motor Liner Based on the Aging of a Curing System.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 1, p. 1, doi. 10.1002/prep.202100135
- By:
- Publication type:
- Article
32
Investigation of the Ablative Properties of an EPDM\Kevlar Insulator in a Solid Rocket Motor.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 1, p. 1, doi. 10.1002/prep.202100051
- By:
- Publication type:
- Article
33
In Memoriam 'Woody' Waesche 1930–2021.
- Published in:
- 2021
- Publication type:
- Obituary
34
The Influence of the Level of Load in the Mixer on the Processability and Mechanical Properties of the Solid Composite Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 12, p. 1878, doi. 10.1002/prep.202100213
- By:
- Publication type:
- Article
35
Shrinking Particle Reaction Model for a Waste Double‐Base Propellant During Alkaline Hydrolysis.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 12, p. 1866, doi. 10.1002/prep.202100206
- By:
- Publication type:
- Article
36
A Study of the Influence of Storage Time of Uncured Propellants on the Final Properties of the Composite in Multi‐Batch Processes on an Industrial Scale.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 9, p. 1458, doi. 10.1002/prep.202100039
- By:
- Publication type:
- Article
37
A Viscoelastic Constitutive Model of Propellant with Pressure Cure.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 7, p. 1036, doi. 10.1002/prep.202000335
- By:
- Publication type:
- Article
38
Effect of Pressure on Mechanical Properties of Composite Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 5, p. 799, doi. 10.1002/prep.202000299
- By:
- Publication type:
- Article
39
Diffusion of Labile Chemical Species in HTPB and HTPB‐XT Solid Propellants and Its Effect over Solid Rocket Motor Properties on Aging – A Study.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 5, p. 782, doi. 10.1002/prep.202000253
- By:
- Publication type:
- Article
40
Cover Picture: Real‐Time Plume Velocity Measurement of Solid Propellant Rocket Motors Using TDLAS Technique (Prop., Explos., Pyrotech. 4/2021).
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 4, p. 511, doi. 10.1002/prep.202180401
- By:
- Publication type:
- Article
41
Real‐Time Plume Velocity Measurement of Solid Propellant Rocket Motors Using TDLAS Technique.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 4, p. 636, doi. 10.1002/prep.202000091
- By:
- Publication type:
- Article
42
Properties of Composite Solid Propellants Containing α‐FeOOH.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2021, v. 46, n. 1, p. 84, doi. 10.1002/prep.202000125
- By:
- Publication type:
- Article
43
Tailoring of Mechanical Properties of Highly Filled Nano‐Aluminized Propellants by Modifying Binder Polymer Microstructure.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 12, p. 1959, doi. 10.1002/prep.202000182
- By:
- Publication type:
- Article
44
Study of Maximum Pressure Rise with Erosive Burning in Multi‐Grain Tubular Solid Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 9, p. 1398, doi. 10.1002/prep.202000063
- By:
- Publication type:
- Article
45
A Short Review about Aerospace Materials Characterization – Bonding Agents and Thermal Insulation.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 8, p. 1175, doi. 10.1002/prep.201900407
- By:
- Publication type:
- Article
46
Effects of Superimposed Pressure on the Mechanical Properties of HTPB Propellant in a Wide Temperature Range.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 8, p. 1216, doi. 10.1002/prep.201900347
- By:
- Publication type:
- Article
47
Combustion of Nanoaluminum and Magnesium in Fuel‐Rich Propellants.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 5, p. 724, doi. 10.1002/prep.201900354
- By:
- Publication type:
- Article
48
Study of Initial Pressure Rise in Multi Grain Solid Propellant Rocket Motor.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 5, p. 741, doi. 10.1002/prep.201900291
- By:
- Publication type:
- Article
49
The Aging Studies of the Low HCl Content Composite Rocket Propellant.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2019, v. 44, n. 9, p. 1193, doi. 10.1002/prep.201900074
- By:
- Publication type:
- Article
50
Exploring New Ways to Solve Old Problems; the Hunt for Alternative Stability Tests.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2019, v. 44, n. 8, p. 980, doi. 10.1002/prep.201800284
- By:
- Publication type:
- Article