It is shown that most promising systems are separate or integral storage type, utilizing water and ammonia as expendable coolants; operation of several control schemes presenting breadth of choice available between minimum refrigerant consumption and minimum of controls and complexity; methods of solving problems posed by weightlessness, high acceleration loading, installation and ground handling; recommendations.
Approach to equipment cooling problems in orbital space vehicle
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1958 Cooling
1958
18 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
AN APPROACH TO EQUIPMENT COOLING PROBLEMS IN AN ORBITAL SPACE VEHICLE
SAE Technical Papers | 1958
|Problems of Environmental Testing of Orbital and Space Vehicle Structures
SAE Technical Papers | 1966
|Medical problems in orbital space flight
Engineering Index Backfile | 1956
|Problems Associated With Environmental Testing of Orbital and Space Vehicle Structures
SAE Technical Papers | 1966
|Space-based orbital transfer vehicle
Elsevier | 1986
|