Back to results
US 4,738,304 AGranted
Direct condensation radiator for spacecraft
AssigneeRCA Corporation
InventorsDouglas R. Chalmers, John J. Pustay
Life of this patent
Estimating the term…
Abstract
Cost and weight of a heat transfer structure for a space vehicle can be reduced by an arrangement of redundant channels for the flow of coolant to heat radiating panels, micrometeroid resisting bumpers located adjacent the channels for preventing penetration by all but the most energetic micrometeroids, and a sensing and control arrangement for sensing the penetration of a coolant channel for shutting off that channel to prevent loss of coolant.
Claims12
A heat transfer arrangement for removing heat from a space vehicle, comprising:
- a vapor plenum adapted for receiving heat-laden coolant vapor for distributing said coolant vapor to a plurality of vapor output ports;
- a liquid plenum including a plurality of input ports for receiving coolant liquid for collecting said coolant liquid and for making said coolant liquid available to a source of waste heat for cooling thereof;
- a thermally conductive pipe including first and second ends and first and second independent fluid channels extending therethrough from said first end to said second end;
- fluid coupling means coupled to said first and second fluid channels at said first and second ends, to said vapor and liquid plenums for controllably coupling coolant fluid through said first and second channels from said vapor plenum to said liquid plenum;
- at least one thermally conductive radiator panel thermally coupled to said pipe and including a portion adapted for substantial black-body radiation into space, whereby said pipe transfers heat from coolant fluid flowing therethrough to said panel for radiation thereof, thereby cooling said fluid, whereby coolant vapor flowing into said first and second channels from said vapor plenum has its latent heat removed, and condenses to a liquid form which in passing towards said liquid plenum further loses sensible heat and decreases in temperature, the environment of said space vehicle being populated by micrometeroids possessing a distribution of kinetic energy ranging from insignificant amounts to amounts sufficient to penetrate the walls of said pipe, which penetration might create an aperture in one of said first and second channels through which said coolant can escape, thereby rendering said heat transfer arrangement ineffective;
- sensing and control means coupled to said fluid coupling means and to said first and second fluid channels for sensing a coolant leak from one of said first and second fluid channels and for controlling said fluid coupling means for decoupling said vapor and liquid plenums from said one of said first and second channels, whereby coolant fluid flow through the other of said first and second channels maintains a substantial amount of capacity of said heat transfer arrangement.
3 more elements
A heat radiator for a space vehicle, comprising:
- an elongated vapor manifold adapted for receiving coolant vapor to be cooled;
- an elongated liquid manifold adapted for receiving cooled liquid coolant, said elongated liquid manifold being arranged in a substantially parallel relationship with said elongated vapor manifold;
- first and second spaced-apart panels which are substantially planar and parallel over a principal portion of their area, said first and second panels being formed from heat-conductive material;
- an elongated pipe-like structure in the form of a thermally conductive multiple-channel pipe including first and second ends and an outer surface, and at least first and second channels extending from said first end to said second end, said elongated pipe-like structure lying in a plane and being located between said first and second panels with a portion of said outer surface thermally bonded to said first panel and another portion of said outer surface thermally bonded to said-second panel, and further being located with said first end adjacent said vapor manifold and said second end adjacent said liquid manifold;
- fluid coupling means coupled to said first and second ends of said pipe-like structure, and to said vapor and liquid manifolds for controllably coupling at least said first and second channels at one end of said first and second ends to said vapor manifold and at the other end of said first and second ends to said liquid manifold, whereby micrometeroids impinging upon said elongated pipe-like structure from a direction approximately normal to said plane are most likely to penetrate through the walls of said pipe-like structure thereby forming an aperture through which said coolant can escape;
- a first elongated bumper located on a side of said first panel remote from said pipe-like structure, said first bumper being dimensioned and located for intercepting micrometeroids impinging on said first panel near said pipe-like structure from a direction approximately normal to said plane;
- a second elongated bumper located on a side of said second panel remote from said pipe-like structure, said second bumper being dimensioned and located for intercepting micrometeroids impinging on said second panel near said pipe-like structure from a direction approximately normal to said plane, whereby a micrometeroid must penetrate one of said first or second bumpers and a corresponding one of said first and second panels before it can transfer a substantial amount of its kinetic energy to said pipe-like structure, but an energetic micrometeroid may nevertheless penetrate through said walls of said pipe-like structure, thereby forming an aperture through which said coolant can escape from one of said first and second channels;
- and
- penetration sensing and control means coupled to said pipe-like structure and to said fluid coupling means for sensing the formation of an aperture through which said coolant can escape and for controlling said coupling means for decoupling at least one of said first and second Channels from both said vapor and liquid manifolds.
6 more elements
Dependencies are inferred from the claim text.