Old Web
English
Sign In
Acemap
>
Paper
>
Combustion Characteristics of Gas Hybrid Rocket using H2O/HNO3 as Oxidizer
Combustion Characteristics of Gas Hybrid Rocket using H2O/HNO3 as Oxidizer
2015
Ikki Suzuki
Takuo Kuwahara
Keywords:
Propellant
Combustion
Rocket
Composite material
Materials science
Aerospace engineering
Correction
Source
Cite
Save
Machine Reading By IdeaReader
1
References
0
Citations
NaN
KQI
[]