Results 61 to 70 of about 17,329 (212)

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles [PDF]

open access: yes
A study was conducted to assess the feasibility of quasi-hybrid solid rocket boosters for advanced Earth-to-orbit vehicles. Thermochemical calculations were conducted to determine the effect of liquid hydrogen addition, solids composition change plus ...
Andreev T.   +7 more
core   +2 more sources

Metal-organic frameworks as hypergolic additives for hybrid rockets. [PDF]

open access: yesChem Sci, 2022
Jobin O   +8 more
europepmc   +1 more source

Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]

open access: yes
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

A Soviet quasi-market for inventions : jet propulsion, 1932–1946 [PDF]

open access: yes
This paper is about how a command system allocated resources under profound uncertainty. The command system was the Soviet economy, the period was Stalin's dictatorship, and the resources were designated for military research & development.
Harrison, Mark
core   +1 more source

Observation of HF Plasma Wave Emissions at Ionospheric Level Using SOunding Rocketes S-310JA-1, 2 in Antarctica

open access: yesAntarctic Record, 1979
Observations of the plasma wave emissions in a high frequency range from 01 to 10 MHz have been made using the lonospheric sounding rockets S-310JA-1, and 2, launched on February 13, 1976 and on February 10,1977, respectively, from Syowa Station in ...
Hiroshi OYA   +2 more
doaj   +1 more source

Conceptual Design of Mars Lander with Novel Impact Intriguing System

open access: yes, 2020
Landing robotic spacecrafts and humans on Mars has become one of the inevitable technological necessities for humans. Effectuating perfect Mars expedition requires landing of enormous cargoes, crewed modules, ascent vehicles, and scientific laboratories.
Annavarapu, Ramesh Naidu   +1 more
core   +1 more source

Development of an Optimized Induction Melting System for Fabricating Paraffin Fuel Grains for Hybrid Rocket Propulsion

open access: yesJournal of Aerospace Technology and Management
This work reports the development of an induction melting system for producing paraffin-based fuel units for hybrid rockets. The system is based in oscillating low-frequency magnetic field to generate heat within the material, enabling a precise ...
José Refugio Martínez   +8 more
doaj  

Investigation of Performance Stability of a Nytrox Hybrid Rocket Propulsion System

open access: yesAerospace
Nitrous oxide is a highly suitable oxidizer for hybrid rockets due to its self-pressurizing properties, moderate cost, and high accessibility. However, its vapor pressure and density are highly dependent on ambient temperature, requiring careful ...
Shih-Sin Wei   +3 more
doaj   +1 more source

Cost analysis of stratospheric albedo modification delivery systems

open access: yesEnvironmental Research Letters, 2012
We perform engineering cost analyses of systems capable of delivering 1–5 million metric tonnes (Mt) of albedo modification material to altitudes of 18–30 km. The goal is to compare a range of delivery systems evaluated on a consistent cost basis.
Justin McClellan, David W Keith, Jay Apt
doaj   +1 more source

Demonstration of dual-thrust capability in hybrid rockets using multi-layered tubular fuel grains

open access: yesFirePhysChem
This study demonstrates the thrust modulation capabilities of a hybrid rocket motor employing a Multi-Layered Tubular (MLT) fuel grain. The MLT configuration involves arranging the fuel grains with distinct regression rates as layers.
Mengu Dinesh   +2 more
doaj   +1 more source

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