Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19670041793

Spin Acceleration Effects on Some Full-Scale Solid Rockets

View original source ↗Export metadata ↓

Abstract

Ballistic propellant combustion alteration and thermal effects due to dynamic spinning observed on solid propellant sounding rockets

Explore related subjects

SOLID PROPELLANT SOUNDING ROCKET BALLISTICS THERMAL EFFECT SPIN DYNAMICS

Keep this discovery

Explore connections, maps & timelines

Lucy, M. H.. 1967-01-01. Spin Acceleration Effects on Some Full-Scale Solid Rockets. https://ntrs.nasa.gov/citations/19670041793

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Particulate damping in solid-propellant combustion instability.

Aluminum powder damping of HF instability in solid propellant combustion in vortex burner

SOLID PROPELLANT↗

NASA NTRS1967

A study of energy release in rocket propellants by a projectile impact method Annual report, 9 May 1966 - 9 May 1967

Projectile impact method for measuring rates of energy release in solid propellants subjected to strong shock waves

SOLID PROPELLANT↗

NASA NTRS1967

Review of thermal radiation from liquid and solid propellant rocket exhausts

Thermal radiation from liquid and solid propellant rocket exhausts

SOLID PROPELLANT↗