Near-future rocket launches could slow ozone recovery. [PDF]
NPJ Clim Atmos SciRevell LE +9 more
europepmc +2 more sources
Worldwide Rocket Launch Emissions 2019: An Inventory for Use in Global Models
Earth and Space ScienceThe rate of rocket launches is accelerating, driven by the rapid global development of the space industry. Rocket launches emit gases and particulates into the stratosphere, where they impact the ozone layer via radiative and chemical processes.
Tyler F. M. Brown +4 more
doaj +1 more source
Technological features of internal making thermal barrier coatings for rocket solid fuel engines
, 2015 Кристина Викторовна Козис +2 more
openalex +2 more sources
Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]
Design issues for lunar ascent and lunar descent rocket engines fueled by aluminum/oxygen propellant produced in situ at the lunar surface were evaluated.
Meyer, Michael L.
core +1 more source
Effects of Nano-Sized Al on the Combustion Performance of Fuel Rich Solid Rocket Propellants
, 2016 Weiqiang Pang +5 more
openalex +2 more sources
Response of selected plant and insect species to simulated solid rocket exhaust mixtures and to exhaust components from solid rocket fuels [PDF]
The effects of solid rocket fuel (SRF) exhaust on selected plant and and insect species in the Merritt Island, Florida area was investigated in order to determine if the exhaust clouds generated by shuttle launches would adversely affect the native ...
Ambrose, J. T. +8 more
core +1 more source
Hybrid Rocket Propulsion for Sounding Rocket Applications [PDF]
A discussion of the H-225K hybrid rocket motor, produced by the American Rocket Company, is given. The H-225K motor is presented in terms of the following topics: (1) hybrid rocket fundamentals; (2) hybrid characteristics; and (3) hybrid ...
core +1 more source
CHOOSING RATIONAL ENGINEERING SOLUTIONS AND DESIGN CRITERIA OF THROTTABLE SOLID FUEL ROCKET ENGINES
, 2022 С.В. Лавров +1 more
openalex +1 more source
Dynamic characteristics of a variable-mass flexible missile: Dynamics of a two-stage variable-mass flexible rocket [PDF]
The dynamic characteristics of two-stage slender elastic body were investigated. The first stage, containing a solid-fuel rocket, possesses variable mass while the second stage, envisioned as a flexible case, contains packaged instruments of constant ...
Bankovskis, J., Meirovitch, L.
core +1 more source