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rockets
Consequently, it can only be detected with instruments on sounding rockets and spacecraft operating above the atmosphere.
      
The data were obtained by two different techniques, rockets and lidars and correspond to different regions of the atmosphere from the upper thermosphere to the stratosphere.
      
The use of a thermionic NPS with a thermal reactor in space technology to supply power to the RMPS offers broad possibilities for interorbital delivery of payloads while using comparatively cheap launch rockets to place spacecraft in a fixed orbit.
      
It is concluded that at the present stage it is best not to use them together with medium-class carrier rockets.
      
Algorithm to predict the kinematic parameters of launcher rockets using telemetric and path measurements
      
Perchlorate is an oxidizer primarily used in solid-fuel rockets, and many sites that processed or used perchlorate are now contaminated.
      
We demonstrate that the one-way speeds of light measured by stable atomic clocks in rockets may not be isotropic, in contrast to the two-way speeds of light.
      
Conventional rockets are not a suitable technology for interstellar missions.
      
Chemical rockets require a very large weight of propellant, travel very slowly compared to light speed, and require significant energy to maintain operation over periods of years.
      
Custom designed experimental packages aboard sounding rockets were utilized for this purpose.
      
High-melting materials for rockets and cosmic missiles
      
We analyze the form of the response of an HF radio signal scattered by the nonstationary disturbances of the electron density Ne caused by acoustic shock-wave disturbances in the upper atmosphere from rockets in the active section of the trajectory.
      
Artificial modification of the ionosphere by launches of rockets which insert space vehicles into orbit
      
Natural Vibration of Pack-Assembled Liquid-Propellant Carrier Rockets
      
A mathematical model has been constructed for numerical calculation of the natural vibration spectrum of pack-assembled liquid-propellant carrier rockets.
      
The inaccuracy of spin-stabilized rockets can be attributed, in part, to the initial motion of the rocket inside the smoothbore launcher.
      
The model material is polyurethane rubber which is similar to the binder material in actual rockets.
      
Such conditions occur in cryogenic propellant rockets on assemblies such as feedlines and turbopumps.
      
La Terre et l'Espace: Rockets, Prisons, Protests and Heritage in Australia and French Guiana
      
The Yugoslavian hail-suppression system uses rockets with 0.4 kg of a pyrotechnical mixture which produces an AgI based aerosol by the process of burning.
      
 

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