Launch Procedures - PowerPoint PPT Presentation

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Launch Procedures

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Launch Procedures No-Go Criteria Winds exceeding 10 knots steady from any direction Cloud ceiling below 10,000 ft AGL Data acquisition systems not operable – PowerPoint PPT presentation

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Title: Launch Procedures


1
Launch Procedures
  • No-Go Criteria
  • Winds exceeding 10 knots steady from any
    direction
  • Cloud ceiling below 10,000 ft AGL
  • Data acquisition systems not operable
  • Rocket subsystems not operable
  •  

2
Launch Procedures (page 2)
  • Pre-Test Preparation
  • Launch rail installed on launch pad.
  • Rocket motor inspection/clearance from Dugway
    Proving Ground personnel
  • Transportation of the rocket motor,
    subassemblies, launch support equipment
    (including power supply) to launch site.
  • Assembly of rocket subsystems at the blockhouse.
  • Pre-launch checks of all electrical and
    mechanical components.
  • Installation of Unity IV Phase II rocket onto
    launch rail.
  • Photo/video camera set-up and field of view
    verification.
  • Final pre-launch checks of electrical and
    mechanical systems.
  • Evacuation of non-essential personnel outside of
    safety footprint.
  • Fill oxidizer tank.
  • Begin launch operations/countdown from the
    blockhouse.

3
Launch Procedures (page 3)
  • Test Events
  •  T-minus countdown and launch (see Timeline and
    Procedures).
  • Rocket ascends to approximately 10,000 ft AGL.
  • Deployment of recovery system 150 ft below
    apogee.
  • Rocket impact downrange.
  • Post Test Events
  • Rocket recovery.
  • Removal of all launch support equipment from
    launch area.
  • Review of flight test data and photo coverage.

4
Timeline and Procedures
  • Time Event ___________________________________
  • t-700 -Arrive at Utah Test and Training Range.
  • -Proceed to the assembly building via Air Force
    vehicles.
  • t-230 -Assembly Team performs maintenance and
    assembles Unity IV Phase II rocket.
  • -Test and check all mechanical and electrical
    components.
  • -Enter atmospheric data into the flight
    controller.
  • t-130 -Transport rocket from assembly building
    to launch pad.
  • -Slide rocket onto the launch rail until stops
    are met.
  • -Raise launch rail to 90 degrees off of
    horizontal and secure launch rail angle and
    support arms.
  • -Assembly Team attaches fins.
  • -All electrical connections are made to the
    ball valve and it is tested and placed in
    correct closed position. Disconnect electrical
    connections to all valves. Solenoid valves are
    manually checked to be in their correct
    position.
  • t-100 -All personnel at the launch pad enter the
    block house.

5
Timeline and Procedures (page 2)
  • Time Event ___________________________________
  • t-030 -Valves are rechecked for their proper
    open/closed positions by eye.
  •           The fill line is connected to the
    self-sealing connect on the upper solenoid
    valve. Vent line connected to vent self-sealing
    connect.
  • -Remove all personnel who are not going to
    remain in the block
  • house from the footprint area.
  • -Remotely fill the rocket oxidizer tank (25ft).
    Monitor pressure and fill level through vent
    line.
  • -Attach the fill line to the first solenoid
    valve connect and keep the the vent line closed.
  • -Fill until vent line sight glass shows liquid
    N2O.
  • -Pressurize Tank to 1200 psig with N2.
  • -Record the final pressure.
  • t-005 -One person will then go to the rocket and
    disconnect the oxidizer
  • fill and vent lines from the solenoid valve and
    vent connects.
  • -Reconnect all electrical connectors to valves.
  • -Seal up access panel.

6
Timeline and Procedures (page 3)
  •  Time Event ___________________________________
  • t-005 Wait for clearance from Range
    Control
  • t-002 Send out warning for countdown. 
  • t-30 sec Verify video equipment is running.
  • t-10 sec Activate the power supply and flip to on
    position.
  • t-0 sec Flip the ignition switch to the on
    position.
  • The flight controller initiates data
    recording.
  • The flight controller lights the igniters for
    six seconds.
  • The flight controller opens the oxidizer
    valves.
  • Verify launch with video monitor.
  • Altitude Event______________________________
  • 150 feet below apogee The flight controller sends
    the signal to separate the nose cone. Nose
    cone chute deploys.
  • Booster section drogue chute deploys.
  • 5000 AGL Booster section main chute deploys.
  • 0 AGL Rocket impacts at 23 fps. Recover the
    rocket.
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