检索

标题
作者
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
Solar thermal propulsion systems with various high-temperature power sources
Finogenov S., Kolomentsev A.
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
To the question of forecasting the technical condition of low-thrust liquid rocket engines
Komlev G., Mitrofanova A.
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function
Torgashin A., Zhujkov D., Nazarov V., Begishev A.
To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines
Dubynin P., Tolstopyatov M., Zuev A., Chernenko V.
IMPROVING THE EFFICIENCY OF MULTIFUNCTIONAL ELECTRIC ROCKET ENGINES
Trifanov I., Kaz’min B., Oborina L., Trifanov V., Savel’eva M.
HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS
Krayev M.
INFLUENCE OF LAUNCH PARAMETERS OF LIQUID ROCKET ENGINE ON THE BALANCE OF AXIAL FORCES IN THE TURBOPUMP
Belayev E., Vorobyev A.
TECHNICAL CHARACTERISTICS OF OXYGEN-HYDROGEN LIQUID ROCKET PROPULSION SYSTEM OF INTERORBITAL SPACE VEHICLE
Borovik I.
SOLAR THERMAL PROPULSION WITH DIFFERENT TYPES OF CONCENTRATOR-ABSORBER SYSTEM
Finogenov S., Kolomentsev A., Nazarov V.
THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION
Finogenov S., Kolomentsev A.
Some units spacecraft balancing
Krushenko G., Golovanova V.
ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS
Belayev E., Vorobyev A.
THE DESIGN OF THE EXPERIMENT AND CREATION OF THE REGRESSION MODEL OF THE SPECIFIC IMPULSE LIQUID ROCKET ENGINE THRUST FROM 10 TO 420 N
Kolomentsev A., Khokhlov A.
The Method of CALCULATION OF THERMAL STATE OF CHAMBER FOR steady state IMPULSE operation OF LIQUID ROCKET ENGINE OF SMALL THRUST
Vorobyev A., Vorobyeva S.
INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE
Belayev E., Vorobyev A.
USE OF DIFFERENT OXIDIZERS FOR AFTERBURNING OF HYDROGEN HEATED BY SOLAR ENERGY IN ROCKET ENGINE
Finogenov S., Kolomentsev A., Kudrin O.
IMPLEMENTATION OF AUTOMATED SYSTEM FOR MANUFACTURING OF PIPELINES OF ROCKET ENGINES
Yartsev E., Nazarov V., Teryaev N.
APPLICATION OF COMBINED POROUS-MESH MATERIALS IN CONSTRUCTIONOF INTRATANK DEVICES OF PROPULISION INSTALLATIONS OF SPACECRAFTS,FINAL STEPS OF CARRIER ROCKETS AND UPPER-STAGES
Sapozhnikov V., Grishko Y., Korol'kov A., Bol'shakov V., Novikov Y., Konstantinov S., Martynov M., Sapozhnikov V., Grischko Y., Korolkov А., Bolshakov V., Novikov Y., Konstantinov S., Martynov M.
THE ALGORITHM FOR ESTIMATING RESERVES OF THE WORKING PROCESS STABILITY IN COMBUSTION CHAMBERS AND GAS GENERATORS OF LIQUID ROCKET ENGINES
Biryukov V., Nazarov V., Tsarapkin R.
1 - 22 的 22 信息

检索提示:

  • 检索的名词区分大小写
  • 常用字词将被忽略
  • 默认情况下只有在查询结果满足所有检索词才返回(例如,隐含AND)
  • 使用OR结合多个检索词,便于查找含有这些检索词的文章,例如education OR research
  • 使用括号来创建更复杂的查询; 例如:archive ((journal OR conference) NOT theses)
  • 使用引号检索一个完整的词组; 例如: "open access publishing"
  • 使用-或者NOT排除一个检索词; 例如:online -politics or online NOT politics
  • 在检索词里使用 *作为通配符匹配任何字符序列; 例如., soci* morality 将符合含有 "sociological" or "societal"的词语
##common.cookie##