Integrated telescopic boom and large deployable reflector
A telescopic boom and reflector assembly for a spacecraft that includes a telescopic boom having a plurality of boom sections that are nested together within a prime batten or where the prime batten is attached to an outermost section of the boom when the boom is in a stowed position, where an innermost and smallest diameter section of the boom is secured to the spacecraft to facilitate testing and integration of the boom and reflector as a unitized assembly. The assembly also includes a reflector having a truss structure configured to allow the reflector to be collapsed into a stowed configuration, where the reflector is mounted to the prime batten. The assembly is configured to be deployed from the spacecraft by releasing the boom in a telescopic manner where the boom sections increase in diameter from the spacecraft outward when the boom is deployed.
1. A boom and reflector assembly for a spacecraft, said assembly comprising:
a telescopic boom including a plurality of boom sections that are nested together within an outer boom section when the boom is in a stowed position, wherein an innermost and smallest diameter section of the boom is secured to the spacecraft;
a reflector including a truss structure that allows the reflector to be collapsed into a stowed configuration, said reflector being mounted to a structure, said structure being secured to the boom, wherein the assembly is configured to be deployed from the spacecraft by releasing the boom in a telescopic manner where the boom sections increase in diameter from the spacecraft outward when the boom is deployed; and
said plurality of boom sections are provided within said structure when the boom is in the stowed position.
2. The assembly according to claim 1 wherein the structure is secured to an outermost boom section.
3. The assembly according to claim 1 wherein the boom, the reflector and the structure are configured as a single unit palletized structure.
4. The assembly according to claim 1 wherein the boom sections have a trapezoidal shape.
5. The assembly according to claim 4 wherein the boom sections have a tubular shape.
6. The assembly according to claim 4 wherein the reflector is mounted along an entire length of the outer structure.
7. The assembly according to claim 4 wherein the reflector is secured to the outer structure in the stowed configuration by a cradle and straps.
8. The assembly according to claim 4 wherein the boom sections are extended in the telescopic manner by a motor driven storable tubular extendable member (STEM) drive mechanism.
9. A boom and reflector assembly for a spacecraft, said assembly comprising:
a telescopic boom including a plurality of boom sections that are nested together within a structure when the boom is in a stowed position, said structure being secured to the boom, wherein an innermost and smallest diameter section of the boom is secured to a motor driven storable tubular extendable member (STEM) drive mechanism mounted to the spacecraft; and
a reflector including a truss structure that allows the reflector to be collapsed into a stowed configuration, said reflector being positioned within a cradle when it is in the stowed configuration and mounted to the structure by straps, wherein the assembly is configured to be deployed from the spacecraft by releasing the boom in a telescopic manner using the STEM drive mechanism where the boom sections increase in diameter from the spacecraft outward when the boom is deployed, and wherein the reflector is deployed after the cradle is released.
10. The assembly according to claim 9 wherein the boom sections have a trapezoidal shape.
11. The assembly according to claim 9 wherein the boom sections have a tubular shape.
12. The assembly according to claim 9 wherein the reflector is mounted along an entire length of the structure.
13. A method for deploying a boom and reflector assembly for a spacecraft, said assembly including a telescopic boom having a plurality of boom sections that are nested together when the boom is in a stowed position, wherein an innermost and smallest diameter section of the boom is secured to the spacecraft, and a reflector including a truss structure that allows the reflector to be collapsed into a stowed configuration, said reflector being mounted to a structure, said structure being secured to the boom, said plurality of boom sections provided within said structure when the boom is in the stowed position, said method comprising:
extending the boom in a telescopic manner so that the boom sections get increasingly larger in diameter the farther they are away from the spacecraft; and
deploying the reflector.
14. The method according to claim 13 wherein the structure is secured to an outermost boom section.
15. The method according to claim 13 wherein the boom, the reflector and the structure are configured as a single unit palletized structure.
16. The method according to claim 13 wherein the boom sections are extended in the telescopic manner by a motor driven storable tubular extendable member (STEM) drive mechanism.