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BOOSTERS

List of hybrid boosters developed and tested by Copenhagen Suborbitals

DATE ENGINE TYPE OXIDIZER FUEL
2010-05-16HEAT-1XPLOXPolyurethane
2010-03-20HATVLOXPolyurethane
2010-03-05HATVLOX (BLOWDOWN)
2010-02-28HEAT-1XLOXParaffin
2009-12-13HATVLOXParaffin
2009-10-17HATVLOXParaffin
2009-09-20BabyHEATLOXParaffin
2009-09-11BabyHEATLOXParaffin
2009-09-11BabyHEATLOXParaffin
2009-09-05BabyHEATLOXParaffin
2009-09-05BabyHEATLOXParaffin
2009-09-04BabyHEATLOXParaffin
2009-08-07BabyHEATLOXParaffin
2009-06-14HATVLNOXEpoxy
2009-03-08HATVLNOXEpoxy
2009-02-07XLR-2LNOXEpoxy
2008-11-16XLR-2LNOXEpoxy
2008-10-19XLR-2LNOXEpoxy

More general info on hybrid booster rockets here

HEAT BOOSTER

The Hybrid Exo Atmospheric Transporter or HEAT, is a real scale rocket with a 640 mm diameter tube that will function as the final rocket and carrier of the one person spacecraft. The oxydizer for the HATV will be liquid oxygen (LOX). The HEAT booster will finally serve as the transportation vehicle for the man rated spacecraft.

The HEAT booster will burn for about 60 seconds, providing 40kN of thrust, resulting in less than 3-g making the trip feasible for humans to endure in an upright position.



The HEAT booster
Brown=epoxy grain, Red=LOX, Blue=spacecraft






Top section of the HEAT LOX tank (diameter 640 mm)


Peter Madsen working on the HEAT-1X booster LOX injector manifold



Production of graphite Nozzle for HEAT-1X

MORE IMAGES ABOUT THIS


Interior picture of the HEAT-1X, epoxy and parafine casting


HEAT-1X parafine chamber with nozzle

BOOSTER CONTROL AND GUIDANCE

We are currently looking into some "basic" guidance control in order to prevent gravity turn and to minimize the touchdown area. Otherwise, the system is very basic and will rely completely on the laws of aerodynamics. By having a large launching tower, currently being developed, the rocket will be guided by passive rails until it have sufficient velocity to reach its apogee using only static fins.

DESCENT AND RECOVERY

Before the spacecraft goes into a zero gravity parabola, the booster system will be jettisoned. After a while of atmosperic re-enty, the spacecraft will be slowered by a drogue parachute and then 3 main parachutes. Finally the spacecraft will touchdown in water.

HEAT-1X-P TEST, MAY 16, 2010

HEAT 1XP TESTED SUCCESFULLY MAY 16, 2010



More data, video and images coming soon...

HEAT 1X TESTING, FEB 28, 2010

HEAT-1X TEST FIRED WITH SUCCESS FEB 28, 2010
We are ready for launching HEAT-1X and Spacecraft Tycho Brahe-1 June 2010




Morten Olsen and Christoffer Meyer during LOX fueling


Copenhagen Suborbitals HEAT-1X team

IMAGE GALLERY FROM HEAT-1X TEST

Copenhagen Suborbitals: HEAT 1X booster test 28 Feb 2010 from Sonny W. on Vimeo.









More images, video and data coming soon....


HATV-LOX/PARAFINE ENGINE TEST OCTOBER 17, 2009











MORE IMAGES FROM THE TEST - SET 1
MORE IMAGES FROM THE TEST - SET 2
VIDEO - CAM 1
VIDEO - CAM 2
VIDEO - CAM 3
VIDEO - CAM 4

HATV-LOX II ENGINE TEST SUNDAY DEC 13, 2009








The Copenhagen Suborbitals team at the Dec 13 HATV-LOX testing



BABY-HEAT PARAFINE/LOX TEST 4-5 SEP 2009





More images from the test Sep 4-5, 2009:
Image Link01
Image Link02

More videos from the test Sep 4-5, 2009:
Video Link01
Video Link02
Video Link03
Video Link04
Video Link05

BABY-HEAT, PARAFINE/LOX ENGINE, TEST AUG 6, 2009





August 6, 2009 we tested our first LOX/parafine engine

HATV BOOSTER

The Hybrid Atmospheric Test Vehicle or HATV, is a 1/3 scale rocket with a 200 mm diameter tube, that will function as a basic flight test model. The oxydizer for the HATV will be nitrous oxide. This rocket is currently being constructed and a minor hold-down booster were tested two times, with succes, in October and November of 2008.


HATV nozle production


Two HATV rockets almost ready


HATV rocket T-1.7 days before test

HATV BOOSTER TEST MARCH 8, 2009


First HATV test 8 Mar 2009, video montage with timecodes from Sonny W. on Vimeo.

HATV BOOSTER TEST SUNDAY 14, 2009

Sunday June 14, we fired the HATV booster once again in Copenhagen.
The booster test was a complete success.


HATV booster fired June 14, 2009


HATV02 - Full sequence, composite view, true speed with audio

MORE VIDEOS FROM THE HATV02 TEST - JUNE 14
Composite view, booster start, 5% speed
Composite view, whole sequence, 5% speed
Composite view, T+20 to flameout, 5% speed
View from audience, whole sequence
Timelapse from the entire day, 8 hours in 3.5min, 25MB avi


Kristian von Bengtson (left) and Peter Madsen (right) after booster testing




More Images from the HATV booster test, June 14, 2009 here:
Image Link01

XLR-2


De Laval nozzle for the HATV in steel and graphite

Epoxy grain for the HATV



The test booster (XLR-2) for the HATV rocket



Copenhagen Suborbitals (XLR-2) hybrid rocket test, Oct 19th 2008. Photo Sonny W.



Peter Madsen and Kristian von Bengtson shakes hands after finishing the booster.


PRE-HATV BOOSTER (XLR-2) VIDEO


XLR-2 hybrid rocket motor test from Sonny W. on Vimeo.


XLR-2 second static test from Sonny W. on Vimeo.

Copenhagen Suborbitals 2010