Systems and techniques for launching a payload
This disclosure describes various techniques and systems for rapid low-cost access to suborbital and orbital space and accommodation of acceleration of sensitive payloads to space. For example, a distributed gas injection system may be used in a ram accelerator to launch multiple payloads through the atmosphere. Additionally or alternatively, multiple projectiles may assemble during flight through the atmosphere to transfer and/or resources to another projectile.
1. A multiple projectile launch system comprising:
a plurality of launch mechanisms configured to accelerate a respective projectile each;
a first control system configured to coordinate the acceleration of the respective projectiles in the respective plurality of launch mechanisms; and
a second control system, disposed in one or more of the respective projectiles, configured to assemble one or more of the respective projectiles in flight after launch.
2. The multiple projectile launch system of claim 1 , wherein the plurality of launch mechanisms comprises one or more of a ram accelerator, a kinetic energy launch system, a hybrid launch system, a chemical rocket system, an electric propulsion launch system, or combinations thereof.
3. The multiple projectile launch system of claim 1 , wherein the first control system configured to stage a first projectile from a first system and a second projectile in a second system such that the first projectile in the first system experiences a lower g-load than the second projectile in the second system.
4. The multiple projectile launch system of claim 1 , wherein
one or more of the respective projectiles comprises one or more of a tether system, a locking mechanism, a propellant transfer system, or combinations thereof; and
the second control system is configured to activate the one or more of the tether system, the locking mechanism, the propellant transfer system, or combinations thereof to act on at least one other of the respective projectiles.
5. The multiple projectile launch system of claim 1 , further comprising an onsite distribution system configured to, upon request of a user, select and load into two or more of the plurality of launch mechanisms two or more projectiles, and launch the selected and loaded two or more projectiles.