An aerospace housing structure comprising: - an aerospace supporting frame comprising: a) a plurality of rods (2a, 2b, 2c, 2d) each comprising two opposite ends (8a,8b,10b,8c,8d); said rods being arranged so as to define two bases substantially parallel and opposite each other, and two sides, which are substantially parallel and opposite each other and are coupled to each other by said bases; b) a plurality of joint nodes (15,16) that couple said ends in a mutually rotating manner so as to be able to configure said supporting frame between a deployed operating condition and a compacted operating condition; said nodes (15,16) being spaced apart from one another in the deployed operating condition and each being hinged to at least two of said rods (2a,2b,2c,2d); in the compacted operating condition, each of said nodes being placed side by side with two adjacent nodes so as to form, together, two supporting members arranged at opposite longitudinal ends of the supporting frame; wherein, in the compacted operating condition, each of said supporting members is ring-shaped; - covering means (32,49,40), which are removably coupled to said supporting frame when said supporting frame is in the deployed condition and are arranged, at least, at one of said bases and said sides; wherein said covering means comprise a canvas arranged around said supporting frame in the deployed condition. - an aerospace supporting frame comprising: a) a plurality of rods (2a, 2b, 2c, 2d) each comprising two opposite ends (8a,8b,10b,8c,8d); said rods being arranged so as to define two bases substantially parallel and opposite each other, and two sides, which are substantially parallel and opposite each other and are coupled to each other by said bases; b) a plurality of joint nodes (15,16) that couple said ends in a mutually rotating manner so as to be able to configure said supporting frame between a deployed operating condition and a compacted operating condition; said nodes (15,16) being spaced apart from one another in the deployed operating condition and each being hinged to at least two of said rods (2a,2b,2c,2d); in the compacted operating condition, each of said nodes being placed side by side with two adjacent nodes so as to form, together, two supporting members arranged at opposite longitudinal ends of the supporting frame; wherein, in the compacted operating condition, each of said supporting members is ring-shaped; a) a plurality of rods (2a, 2b, 2c, 2d) each comprising two opposite ends (8a,8b,10b,8c,8d); said rods being arranged so as to define two bases substantially parallel and opposite each other, and two sides, which are substantially parallel and opposite each other and are coupled to each other by said bases; b) a plurality of joint nodes (15,16) that couple said ends in a mutually rotating manner so as to be able to configure said supporting frame between a deployed operating condition and a compacted operating condition; said nodes (15,16) being spaced apart from one another in the deployed operating condition and each being hinged to at least two of said rods (2a,2b,2c,2d); in the compacted operating condition, each of said nodes being placed side by side with two adjacent nodes so as to form, together, two supporting members arranged at opposite longitudinal ends of the supporting frame; wherein, in the compacted operating condition, each of said supporting members is ring-shaped; - covering means (32,49,40), which are removably coupled to said supporting frame when said supporting frame is in the deployed condition and are arranged, at least, at one of said bases and said sides; wherein said covering means comprise a canvas arranged around said supporting frame in the deployed condition.